Method of making polymer ammunition cartridge having a two-piece primer insert

The present invention provides ammunition cartridge having a two piece primer insert with a flange, a polymeric middle body extending from the primer insert to a cylindrical middle body coupling region, and a polymeric projectile end having a projectile aperture mated to the polymeric middle body.

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Description
CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a Divisional Application of and claims priority based on U.S. patent application Ser. No. 15/959,657, filed Apr. 23, 2018, which is a Continuation Application of U.S. patent application Ser. No. 15/801,837, filed Nov. 2, 2017, now U.S. Pat. No. 9,976,840, which is a Continuation Application of U.S. patent application Ser. No. 15/064,807, filed Mar. 9, 2016, now U.S. Pat. No. 9,835,427, the contents of which are all incorporated by reference herein in their entirety.

TECHNICAL FIELD OF THE INVENTION

The present invention relates in general to the field of ammunition, specifically to polymer ammunition cartridges having a primer inserts made by joining 2 or more portions.

STATEMENT OF FEDERALLY FUNDED RESEARCH

Not Applicable.

INCORPORATION-BY-REFERENCE OF MATERIALS FILED ON COMPACT DISC

Not Applicable.

BACKGROUND OF THE INVENTION

Without limiting the scope of the invention, its background is described in connection with lightweight polymer cartridge casing ammunition. Conventional ammunition cartridge casings for rifles and machine guns, as well as larger caliber weapons, are made from brass, which is heavy, expensive, and potentially hazardous. There exists a need for an affordable lighter weight replacement for brass ammunition cartridge cases that can increase mission performance and operational capabilities. Lightweight polymer cartridge casing ammunition must meet the reliability and performance standards of existing fielded ammunition and be interchangeable with brass cartridge casing ammunition in existing weaponry. Reliable cartridge casings manufacturing requires uniformity (e.g., bullet seating, bullet-to-casing fit, casing strength, etc.) from one cartridge to the next in order to obtain consistent pressures within the casing during firing prior to bullet and casing separation to create uniformed ballistic performance. Plastic cartridge casings have been known for many years but have failed to provide satisfactory ammunition that could be produced in commercial quantities with sufficient safety, ballistic, handling characteristics, and survive physical and natural conditions to which it will be exposed during the ammunition's intended life cycle; however, these characteristics have not been achieved.

For example, U.S. Pat. No. 7,441,504 discloses a base for a cartridge casing body for an ammunition article, the base having an ignition device; an attachment device at one end thereof, the attachment device being adapted to the base to a cartridge casing body; wherein the base is made from plastic, ceramic, or a composite material.

U.S. Pat. No. 7,610,858 discloses an ammunition cartridge assembled from a substantially cylindrical polymeric cartridge casing body; and a cylindrical polymeric middle body component with opposing first and second ends, wherein the first end has a coupling element that is a mate for the projectile-end coupling element and joins the first end of the middle body component to the second end of the bullet-end component, and the second end is the end of the casing body opposite the projectile end and has a male or female coupling element; and a cylindrical cartridge casing head-end component with an essentially closed base end with a primer hole opposite an open end with a coupling element that is a mate for the coupling element on the second end of the middle body and joins the second end of the middle body component to the open end of the head-end component.

Shortcomings of the known methods of producing plastic or substantially plastic ammunition include the possibility of the projectile being pushed into the cartridge casing, the bullet pull being too light such that the bullet can fall out, the bullet pull being too insufficient to create sufficient chamber pressure, the bullet pull not being uniform from round to round, and portions of the cartridge casing breaking off upon firing causing the weapon to jam or damage or danger when subsequent rounds are fired or when the casing portions themselves become projectiles. To overcome the above shortcomings, improvements in cartridge case design and performance polymer materials are needed.

BRIEF SUMMARY OF THE INVENTION

The present invention provides an ammunition cartridge having a two piece primer insert comprising: a two piece primer insert (32) comprising: an upper primer insert portion (56) connected to a lower primer insert portion (58), wherein the upper primer insert portion (56) comprises an upper primer bottom surface (34), an upper primer aperture (33) through the upper primer bottom surface (34), and a substantially cylindrical coupling element (30) extending away from the upper primer bottom surface (34), wherein the lower primer insert portion (58) comprises: a lower primer bottom surface (35) opposite a lower primer top surface (36), a primer recess (38) in the lower primer top surface (36) that extends toward the lower primer bottom surface (35) and adapted to fit a primer, a lower flash hole aperture (37) through the lower primer bottom surface (35), wherein the lower flash hole aperture (37) is larger than the upper primer aperture (33) to form a flash hole groove (39) in the primer recess (38); a polymeric middle body extending from a middle body coupling region over the two piece primer insert and into the flash hole groove to form a flash hole, wherein the polymeric middle body comprises a first polymer; a polymeric nose portion comprising a nose coupler connected to the middle body coupling region, a shoulder extending from the nose coupler, a neck extending from the shoulder and a projectile aperture in the neck, wherein the nose portion comprises a second polymer; and a propellant chamber defined between the flash hole and the projectile aperture. The two piece primer insert may include a primer flash aperture groove positioned in the primer recess around the primer flash aperture and the first polymer composition extends into the primer flash aperture to form a flash hole. The first polymer composition, the second polymer composition or both comprise a nylon polymer. The first polymer composition, the second polymer composition or both comprise a fiber-reinforced polymeric composite e.g., between about 10 and about 70 wt % glass fiber fillers, mineral fillers, or mixtures thereof. The bullet aperture may include one or more cannelures formed on an inner circumferential surface of the bullet aperture. The substantially cylindrical coupling region and the polymeric bullet-end coupling may be welded or bonded together. The first polymer composition, the second polymer composition or both may be polyurethane prepolymer, cellulose, fluoro-polymer, ethylene inter-polymer alloy elastomer, ethylene vinyl acetate, nylon, polyether imide, polyester elastomer, polyester sulfone, polyphenyl amide, polypropylene, polyvinylidene fluoride or thermoset polyurea elastomer, acrylics, homopolymers, acetates, copolymers, acrylonitrile-butadinen-styrene, thermoplastic fluoro polymers, inomers, polyamides, polyamide-imides, polyacrylates, polyatherketones, polyaryl-sulfones, polybenzimidazoles, polycarbonates, polybutylene, terephthalates, polyether imides, polyether sulfones, thermoplastic polyimides, thermoplastic polyurethanes, polyphenylene sulfides, polyethylene, polypropylene, polysulfones, polyvinylchlorides, styrene acrylonitriles, polystyrenes, polyphenylene, ether blends, styrene maleic anhydrides, polycarbonates, allyls, aminos, cyanates, epoxies, phenolics, unsaturated polyesters, bismaleimides, polyurethanes, silicones, vinylesters, urethane hybrids, polyphenylsulfones, copolymers of polyphenylsulfones with polyethersulfones or polysulfones, copolymers of poly-phenylsulfones with siloxanes, blends of polyphenylsulfones with polysiloxanes, poly(etherimide-siloxane) copolymers, blends of polyetherimides and polysiloxanes, and blends of polyetherimides and poly(etherimide-siloxane) copolymers. The projectile may be a 223, .243, .25-06, .270, .300, .308, .338, .30-30, .30-06, .45-70 or .50-90, 50 caliber, 45 caliber, 380 caliber or 38 caliber, 5.56 mm, 6 mm, 7 mm, 7.62 mm, 8 mm, 9 mm, 10 mm, 12.7 mm, 14.5 mm, 14.7 mm, 20 mm, 25 mm, 30 mm, 40 mm, 57 mm, 60 mm, 75 mm, 76 mm, 81 mm, 90 mm, 100 mm, 105 mm, 106 mm, 115 mm, 120 mm, 122 mm, 125 mm, 130 mm, 152 mm, 155 mm, 165 mm, 175 mm, 203 mm or 460 mm, 4 inch, 4.2 inch or 8 inch. The projectile may have a frustoconical shaped nose. The frustoconical shape may be a cavity to form a hollow point projectile. The projectile may have a spritzer shaped nose and/or a boattail shaped base. The upper primer insert portion, the lower primer insert portion or both may be independently formed by metal injection molding, polymer injection molding, stamping, milling, molding, machining, punching, fine blanking, smelting, or any other method that will form insert portions that may be joined together to form a primer insert. The upper primer insert portion, the lower primer insert portion or both independently comprises a polymer, a metal, an alloy, or a ceramic alloy. The ammunition of claim 4, wherein the upper primer insert portion and the lower primer insert portion may be made of the same material or different materials. A flash hole groove may extend circumferentially about the upper primer aperture or the lower primer aperture.

The present invention includes an ammunition cartridge having a three piece primer insert comprising: an upper primer insert portion comprising an upper primer bottom surface opposite an upper primer top surface, an upper primer aperture through the upper primer bottom surface and the an upper primer top surface; a flash hole groove that extends circumferentially about the upper primer aperture on the upper primer bottom surface, a substantially cylindrical coupling element extending away from the upper primer top surface, and an interior surface inside the substantially cylindrical coupling element; a lower primer insert portion comprising a lower primer bottom surface opposite a lower primer top surface, a primer recess in the lower primer top surface that extends toward the lower primer bottom surface and adapted to fit a primer, and a lower primer aperture through the lower primer bottom surface; an insert joint that links the upper primer bottom surface and the lower primer bottom surface to align the lower primer aperture and form a primer insert; a flange portion comprising a flange top surface opposite a flange bottom surface, a flange primer aperture extending from the flange top surface to the flange bottom surface, and a flange that extends circumferentially about an outer edge of the flange bottom surface, wherein the flange is adapted to receive a polymer overmolding; and a flange joint that links the flange bottom surface and the lower primer bottom surface to align the flange primer aperture and the lower primer aperture to form a primer insert, wherein the insert joint is smelted, sintered, adhesive bonded, laser welded, ultrasonic welded, friction spot welded, or friction stir welded, wherein the flange joint is smelted, sintered, adhesive bonded, laser welded, ultrasonic welded, friction spot welded, and friction stir welded, wherein the upper primer insert portion, the lower primer insert portion or both independently formed by metal injection molding, polymer injection molding, stamping, milling, molding, machining, punching, fine blanking, smelting, or any other method that will form insert portions that may be joined together to form a primer insert; a substantially cylindrical polymeric middle body extending from the substantially cylindrical primer insert to a cylindrical middle body coupling region molded from a first polymer, wherein the first polymer is molded over the flange, the inner circumferential surface and the outer surface and extends to the cylindrical middle body coupling region; a substantially cylindrical polymeric projectile end mated to the substantially cylindrical polymeric middle body, wherein the substantially cylindrical polymeric projectile end comprises a projectile end coupling region that extends to a shoulder region that reduces to a neck region having a projectile aperture wherein the projectile end coupling region couples to the middle body coupling region; and a propellant chamber defined between the primer flash aperture and the projectile aperture.

The present invention includes an ammunition cartridge having a two piece primer insert comprising: a two piece insert comprising: an upper primer insert portion comprising an upper primer bottom surface, an upper primer aperture through the upper primer bottom surface; a substantially cylindrical coupling element extending away from the upper primer bottom surface, and an interior surface inside the substantially cylindrical coupling element; a lower primer insert portion comprising a lower primer bottom surface opposite a lower primer top surface, a flash hole groove that extends circumferentially about the upper primer aperture or the lower primer aperture, and the first polymer composition extends into the primer flash aperture to form a flash hole, a primer recess in the lower primer top surface that extends toward the lower primer bottom surface and adapted to fit a primer, a lower primer aperture through the lower primer bottom surface, and a flange that extends circumferentially about an outer edge of the lower primer top surface, wherein the flange is adapted to receive a polymer overmolding; and an insert joint that links the upper primer bottom surface and the lower primer bottom surface to align the lower primer aperture and form a primer insert; a substantially cylindrical polymeric middle body extending from the substantially cylindrical primer insert to a cylindrical middle body coupling region molded from a first polymer, wherein the first polymer is molded over the flange, the inner circumferential surface and the outer surface and extends to the cylindrical middle body coupling region; a substantially cylindrical polymeric projectile end mated to the substantially cylindrical polymeric middle body, wherein the substantially cylindrical polymeric projectile end comprises a projectile end coupling region that extends to a shoulder region that reduces to a neck region having a projectile aperture wherein the projectile end coupling region couples to the middle body coupling region; and a propellant chamber defined between the primer flash aperture and the projectile aperture.

BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS

For a more complete understanding of the features and advantages of the present invention, reference is now made to the detailed description of the invention along with the accompanying figures and in which:

FIG. 1 depicts a side, cross-sectional view of a polymeric cartridge case according to one embodiment of the present invention;

FIG. 2 depicts a side, cross-sectional view of a portion of the polymeric cartridge case according to one embodiment of the present invention;

FIG. 3 depicts a side, cross-sectional view of a portion of the polymeric cartridge case having a two piece primer insert.

FIG. 4 depicts a side, cross-sectional view of a portion of the polymeric cartridge case having a two piece primer insert and a diffuser.

FIGS. 5A-5H depict different embodiment of the diffuser of the present invention.

FIGS. 6A-6D depicts a side, cross-sectional view of a two piece primer insert used in a polymeric cartridge case.

FIGS. 7A-7B depicts a side, cross-sectional view of a stamped two piece primer insert used in a polymeric cartridge case.

FIGS. 8A-8C depicts a side, cross-sectional view of a two piece primer insert having a tab and groove configuration used in a polymeric cartridge case.

FIGS. 9A-9B depicts a side, cross-sectional view of a three piece primer insert configuration used in a polymeric cartridge case.

FIG. 10 depicts a perspective view of a two piece primer insert used in a polymeric cartridge case.

DETAILED DESCRIPTION OF THE INVENTION

While the making and using of various embodiments of the present invention are discussed in detail below, it should be appreciated that the present invention provides many applicable inventive concepts that can be embodied in a wide variety of specific contexts. The specific embodiments discussed herein are merely illustrative of specific ways to make and use the invention and do not delimit the scope of the invention.

Reliable cartridge manufacture requires uniformity from one cartridge to the next in order to obtain consistent ballistic performance. Among other considerations, proper bullet seating and bullet-to-casing fit is required. In this manner, a desired pressure develops within the casing during firing prior to bullet and casing separation. Historically, bullets employ a cannelure, which is a slight annular depression formed in a surface of the bullet at a location determined to be the optimal seating depth for the bullet. In this manner, a visual inspection of a cartridge could determine whether or not the bullet is seated at the proper depth. Once the bullet is inserted into the casing to the proper depth, one of two standard procedures is incorporated to lock the bullet in its proper location. One method is the crimping of the entire end of the casing into the cannelure. A second method does not crimp the casing end; rather the bullet is pressure fitted into the casing.

The polymeric ammunition cartridges of the present invention are of a caliber typically carried by soldiers in combat for use in their combat weapons. The present invention is not limited to the described caliber and is believed to be applicable to other calibers as well. This includes various small and medium caliber munitions, including 5.56 mm, 7.62 mm, 308, 338, 3030, 3006, and 0.50 caliber ammunition cartridges, as well as medium/small caliber ammunition such as 380 caliber, 38 caliber, 9 mm, 10 mm, 20 mm, 25 mm, 30 mm, 40 mm, 45 caliber and the like. The projectile and the corresponding cartridge may be of any desired size, e.g., .223, .243, .25-06, .270, .300, .308, .338, .30-30, .30-06, .45-70 or .50-90, 50 caliber, 45 caliber, 380 caliber or 38 caliber, 5.56 mm, 6 mm, 7 mm, 7.62 mm, 8 mm, 9 mm, 10 mm, 12.7 mm, 14.5 mm, 14.7 mm, 20 mm, 25 mm, 30 mm, 40 mm, 57 mm, 60 mm, 75 mm, 76 mm, 81 mm, 90 mm, 100 mm, 105 mm, 106 mm, 115 mm, 120 mm, 122 mm, 125 mm, 130 mm, 152 mm, 155 mm, 165 mm, 175 mm, 203 mm or 460 mm, 4.2 inch or 8 inch. The cartridges, therefore, are of a caliber between about 0.05 and about 5 inches. Thus, the present invention is also applicable to the sporting goods industry for use by hunters and target shooters.

The present invention includes primer inserts that are made as a multi-piece insert. In one embodiment the multi-piece insert is a 2 piece insert but may be a 3, 4, 5, or 6 piece insert. Regardless of the number of pieces the multi-piece insert each piece may be of similar or dissimilar materials that are connected to form a unitary primer insert. The portions of the primer insert may be constructed from dissimilar materials including metal-to-metal, polymer-to-polymer and metal-to-polymer joints. The individual pieces may be joined using various methods including smelting, sintering, adhesive bonding, welding techniques that joining dissimilar materials, including laser welding, ultrasonic welding, friction spot welding, and friction stir welding. The method of connecting the individual pieces to form a unitary insert will depend on the materials being joined. For example, a metal insert may is constructed from 2 or more metal pieces with similar melting points are joined together to form a unitary insert through sintering.

The substantially cylindrical primer insert 32 includes at least an upper primer insert portion 56 and a lower primer insert portion 58 joined at insert joint 60. Although, there can be 3, 4, 5, 6, or more portions. In addition the portions may be in the vertical axis instead of the horizontal axis as shown in the figures. For example, the interior portion may be a first portion, the outer portion a second portion and the lower section may be a third portion, and the outer portion a fourth portion.

Regardless of the number of section each portion may be made from a single material that is milled, stamped, forged, machined, molded, cast or other method of forming a primer insert portion.

FIG. 1 depicts a side, cross-sectional view of a portion of a polymeric cartridge case having a two piece primer insert. A cartridge 10 is shown manufactured with a polymer casing 12 showing a propellant chamber 14 with projectile aperture at the forward end opening 16. The polymer casing 12 has a substantially cylindrical open-ended polymeric bullet-end 18 extending from forward end opening 16 rearward to opposite end 20. The bullet-end component 18 may be formed with the coupling end 22 formed on the end 20. The coupling end 22 is shown as a female element, but may also be configured as a male element in alternate embodiments of the invention. The forward end of bullet-end component 18 has a shoulder 24 forming chamber neck 26. The bullet-end component typically has a wall thickness between about 0.003 and about 0.200 inches; more preferably between about 0.005 and about 0.150; and more preferably between about 0.010 and about 0.050 inches.

The middle body component 28 is connected to a substantially cylindrical coupling element 30 of the substantially cylindrical insert 32. The coupling element 30, as shown may be configured as a male element, however, all combinations of male and female configurations is acceptable for the coupling elements 30 and the coupling end 22 in alternate embodiments of the invention. The coupling end 22 of bullet-end component 18 fits about and engages the coupling element 30 of a substantially cylindrical insert 32.

The substantially cylindrical primer insert 32 has an upper primer insert portion 56 and a lower primer insert portion 58 joined at insert joint 60. The upper primer insert portion 56 may be of the same or different materials than lower primer insert portion 58. The insert joint 60 mates the upper primer insert portion 56 and the lower primer insert portion 58 while retaining the primer flash hole 40. The insert joint 60 mates the upper primer insert portion 56 and the lower primer insert portion 58 by welding or bonding using solvent, adhesive, spin-welding, vibration-welding, ultrasonic-welding or laser-welding techniques. In addition multiple methods may be used to increases the joint strength. The upper primer insert portion 56 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 38 and extends through the bottom surface 34 into the propellant chamber 14. The coupling end 22 extends the polymer through the primer flash hole 40 to form an aperture coating 42 while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14 to provide support and protection about the primer flash hole 40. When contacted the coupling end 22 interlocks with the substantially cylindrical coupling element 30, through the coupling element 30 that extends with a taper to a smaller diameter at the tip 44 to form a physical interlock between substantially cylindrical insert 32 and middle body component 28. The polymer casing 12 also has a substantially cylindrical open-ended middle body component 28. The middle body component extends from a forward end opening 16 to the coupling element 22. The middle body component typically has a wall thickness between about 0.003 and about 0.200 inches; and more preferably between about 0.005 and about 0.150 inches; and more preferably between about 0.010 and about 0.050 inches. The bullet-end 16, middle body 18 and bottom surface 34 define the interior of propellant chamber 14 in which the powder charge (not shown) is contained. The interior volume of the propellant chamber 14 may be varied to provide the volume necessary for complete filling of the chamber 14 by the propellant chosen so that a simplified volumetric measure of propellant can be utilized when loading the cartridge. Either a particulate or consolidated propellant can be used. The lower primer insert portion 58 also has a flange 46 and a primer recess 38 formed therein for ease of insertion of the primer (not shown). The primer recess 38 is sized so as to receive the primer (not shown) in an interference fit during assembly. A primer flash hole 40 communicates through the bottom surface 34 of substantially cylindrical insert 32 into the propellant chamber 14 so that upon detonation of primer (not shown) the powder (not shown) in propellant chamber 14 will be ignited.

The projectile (not shown) is held in place within chamber case neck 26 at forward opening 16 by an interference fit. Mechanical crimping of the forward opening 16 can also be applied to increase the bullet pull force holding the bullet (not shown) in place. The bullet (not shown) may be inserted into place following the completion of the filling of propellant chamber 14. The projectile (not shown) can also be injection molded directly onto the forward opening 16 prior to welding or bonding together using solvent, adhesive, spin-welding, vibration-welding, ultrasonic-welding or laser-welding techniques. The welding or bonding increases the joint strength so the casing can be extracted from the hot gun casing after firing at the cook-off temperature.

The bullet-end 18 and bullet components can then be welded or bonded together using solvent, adhesive, spin-welding, vibration-welding, ultrasonic-welding or laser-welding techniques. The welding or bonding increases the joint strength so the casing can be extracted from the hot gun casing after firing at the cook-off temperature. An optional first and second annular groove (cannelures) may be provided in the bullet-end in the interlock surface of the male coupling element to provide a snap-fit between the two components. The cannelures formed in a surface of the bullet at a location determined to be the optimal seating depth for the bullet. The bullet is inserted into the casing to the depth to lock the bullet in its proper location. One method is the crimping of the entire end of the casing into the cannelures. The bullet-end and middle body components can then be welded or bonded together using solvent, adhesive, spin-welding, vibration-welding, ultrasonic-welding or laser-welding techniques. The welding or bonding increases the joint strength so the casing can be extracted from the hot gun casing after firing at the cook-off temperature.

FIG. 2 depicts a side, cross-sectional view of a portion of the polymeric cartridge case having a two piece primer insert. The substantially cylindrical primer insert 32 has an upper primer insert portion 56 and a lower primer insert portion 58 joined at insert joint 60. The upper primer insert portion 56 may be of the same or different materials than lower primer insert portion 58. The upper primer insert portion 56 mates to the lower primer insert portion 58 at insert joint 60 while retaining the primer flash hole 40 and the primer recess 38. The insert joint 60 may connect the upper primer insert portion 56 and the lower primer insert portion 58 by welding or bonding using solvent, adhesive, spin-welding, vibration-welding, ultrasonic-welding or laser-welding techniques. In addition, multiple methods may be used to increase the joint strength. The upper primer insert portion 56 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. The coupling element 30 extends with a taper to a smaller diameter at the tip 44. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 38 and extends through the bottom surface 34 into the propellant chamber 14. The coupling end 22 of the middle body extends the polymer through the primer flash hole 40 to form an aperture coating 42 while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14 to provide support and protection about the primer flash hole 40. When over-molded the coupling end 22 interlocks with the substantially cylindrical coupling element 30. The coupling element 30 extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 to the middle body component. The substantially cylindrical insert 32 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 38 and extends through the bottom surface 34 into the propellant chamber 14. The coupling end 22 extends the polymer through the primer flash hole 40 to form an aperture coating 42 while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14 to provide support and protection about the primer flash hole 40. When contacted the coupling end 22 interlocks with the substantially cylindrical coupling element 30, through the coupling element 30 that extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 and the middle body component 28.

FIG. 3 depicts a side, cross-sectional view of a portion of the polymeric cartridge case having a two piece primer insert. The substantially cylindrical primer insert 32 has an upper primer insert portion 56 and a lower primer insert portion 58 joined at insert joint 60. The upper primer insert portion 56 may be of the same or different materials than lower primer insert portion 58. The upper primer insert portion 56 mates to the lower primer insert portion 58 at insert joint 60 while retaining the primer flash hole 40 and the primer recess 38. The insert joint 60 may connect the upper primer insert portion 56 and the lower primer insert portion 58 by welding or bonding using solvent, adhesive, spin-welding, vibration-welding, ultrasonic-welding or laser-welding techniques. In addition, multiple methods may be used to increase the joint strength. The upper primer insert portion 56 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. The coupling element 30 extends with a taper to a smaller diameter at the tip 44. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 38 and extends through the bottom surface 34 into the propellant chamber 14. The coupling end 22 of the middle body extends the polymer up to the primer flash hole 40 while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14. When over-molded the coupling end 22 interlocks with the substantially cylindrical coupling element 30. The coupling element 30 extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 to the middle body component. The substantially cylindrical insert 32 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 38 and extends through the bottom surface 34 into the propellant chamber 14. The coupling end 22 extends the polymer through the primer flash hole 40 to form an aperture coating 42 while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14 to provide support and protection about the primer flash hole 40. When contacted the coupling end 22 interlocks with the substantially cylindrical coupling element 30, through the coupling element 30 that extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 and the middle body component 28.

FIG. 4 depicts a side, cross-sectional view of a portion of the polymeric cartridge case having a two piece primer insert and a diffuser. The substantially cylindrical primer insert 32 has an upper primer insert portion 56 and a lower primer insert portion 58 joined at insert joint 60. The upper primer insert portion 56 may be of the same or different materials than lower primer insert portion 58. The upper primer insert portion 56 mates to the lower primer insert portion 58 at insert joint 60 while retaining the primer flash hole 40 and the primer recess 38. The insert joint 60 may connect the upper primer insert portion 56 and the lower primer insert portion 58 by welding or bonding using solvent, adhesive, spin-welding, vibration-welding, ultrasonic-welding or laser-welding techniques. In addition, multiple methods may be used to increase the joint strength. The upper primer insert portion 56 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. The coupling element 30 extends with a taper to a smaller diameter at the tip 44. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 38 and extends through the bottom surface 34 into the propellant chamber 14. The coupling end 22 of the middle body extends the polymer through the primer flash hole 40 to form an aperture coating 42 while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14 to provide support and protection about the primer flash hole 40. When over-molded the coupling end 22 interlocks with the substantially cylindrical coupling element 30. The coupling element 30 extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 to the middle body component. The substantially cylindrical insert 32 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 38 and extends through the bottom surface 34 into the propellant chamber 14. The coupling end 22 extends the polymer through the primer flash hole 40 to form an aperture coating 42 while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14 to provide support and protection about the primer flash hole 40. When contacted the coupling end 22 interlocks with the substantially cylindrical coupling element 30, through the coupling element 30 that extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 and the middle body component 28. The diffuser 50 includes a diffuser aperture 52 and a diffuser aperture extension 54 that aligns with the primer flash hole 40. The diffuser 50 diverts the combustion effect away from the over-molded polymer material of the middle body component 28. The affects being the impact from igniting the primer as far as pressure and heat to divert the energy of the primer off of the polymer and directing it to the flash hole. The diffuser 50 can be between 0.004 to 0.010 inches (e.g., 0.0001, 0.0002, 0.0003, 0.0004, 0.0005, 0.0006, 0.0007, 0.0008, 0.0009, 0.001, 0.002, 0.003, 0.004, 0.005, 0.006, 0.007, 0.008, 0.009, 0.010, 0.011, 0.012, 0.013, 0.014, or 0.015) in thickness and made from metal, polymer, composite, or other material, e.g., half hard brass. For example, the diffuser 50 can be between about 0.005 inches thick for a 5.56 diffuser 50. The outer diameter of the diffuser for a 5.56 or 223 case is 0.173 and the inner diameter is 0.080. The diffuser could be made of any material that can withstand the energy from the ignition of the primer, e.g., alloys, metals, steel, stainless, cooper, aluminum, resins and polymers. The diffuser 50 can be produce in “T”, ‘L” or “I” shape by drawing the material by MIM, PIM, milling, machining, or using a stamping and draw die. In the “T”, ‘L” or “I” shape diffusers the center ring can be 0.005 to 0.010 tall and the outer diameter is 0.090 and the inner diameter 0.080, individually 0.001, 0.002, 0.003, 0.004, 0.005, 0.006, 0.007, 0.008, 0.009, 0.010, 0.011, 0.012, 0.013, 0.014, 0.015, 0.02, 0.02.5, 0.03, 0.04, 0.05, 0.06, 0.07, 0.08, 0.09, 0.1, or 0.2.

FIGS. 5A-5H depict different embodiment of the diffuser of the present invention.

FIG. 6A depict a side, cross-sectional view of a two piece primer insert used in a polymeric cartridge case. The two piece primer insert (32) comprises: an upper primer insert portion (56) connected to a lower primer insert portion (58), wherein the upper primer insert portion (56) comprises an upper primer bottom surface (34), an upper primer aperture (33) through the upper primer bottom surface (34), and a substantially cylindrical coupling element (30) extending away from the upper primer bottom surface (34), wherein the lower primer insert portion (58) comprises: a lower primer bottom surface (35) opposite a lower primer top surface (36), a primer recess (38) in the lower primer top surface (36) that extends toward the lower primer bottom surface (35) and adapted to fit a primer, a lower flash hole aperture (37) through the lower primer bottom surface (35), wherein the lower flash hole aperture (37) is larger than the upper primer aperture (33) to form a flash hole groove (39) in the primer recess (38)

FIGS. 6B-6D depict a side, cross-sectional view of a two piece primer insert used in a polymeric cartridge case. The substantially cylindrical primer insert 32 has an upper primer insert portion 56 and a lower primer insert portion 58 joined at insert joint 60. The upper primer insert portion 56 may be of the same or different materials than lower primer insert portion 58. The upper primer insert portion 56 mates to the lower primer insert portion 58 at insert joint 60 while retaining the primer flash hole 40 and the primer recess 38. The insert joint 60 may connect the upper primer insert portion 56 and the lower primer insert portion 58 by welding or bonding using solvent, adhesive, spin-welding, vibration-welding, ultrasonic-welding or laser-welding techniques. In addition, multiple methods may be used to increase the joint strength. The upper primer insert portion 56 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. The coupling element 30 extends with a taper to a smaller diameter at the tip 44. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 38 and extends through the bottom surface 34 into the propellant chamber 14. The coupling end 22 of the middle body extends the polymer through the primer flash hole 40 to form an aperture coating (not shown) while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14 to provide support and protection about the primer flash hole 40. When over-molded the coupling end 22 interlocks with the substantially cylindrical coupling element 30. The coupling element 30 extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 to the middle body component. The substantially cylindrical insert 32 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 28 and extends through the bottom surface 34 into the propellant chamber 14. The coupling end 22 extends the polymer through the primer flash hole 40 to form an aperture coating (not shown) while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14 to provide support and protection about the primer flash hole 40. When contacted the coupling end 22 interlocks with the substantially cylindrical coupling element 30, through the coupling element 30 that extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 and the middle body component 28.

The present invention provides a method of making a multi-piece insert that is joined to form a unitary insert that can be overmolded into an ammunition cartridge. The individual components of the insert may be made may any method provided the insert is functional. For example, the individual pieces may be stamped or milled and then connected. The connection can also be of any mechanism that is available currently that produces a viable insert with the desired joint strength. For example, the joint may be welded or soldered as in FIG. 7A or riveted or coined as in FIG. 7B.

FIGS. 7A-7B depict a side, cross-sectional view of a two piece primer insert used in a polymeric cartridge case. The substantially cylindrical primer insert 32 has an upper primer insert portion 56 and a lower primer insert portion 58 joined at insert joint 60. The upper primer insert portion 56 may be of the same or different materials than lower primer insert portion 58. The upper primer insert portion 56 mates to the lower primer insert portion 58 at insert joint 60 while retaining the primer flash hole 40 and the primer recess 38. The insert joint 60 may connect the upper primer insert portion 56 and the lower primer insert portion 58 by soldering, welding spin-welding, vibration-welding, ultrasonic-welding or laser-welding techniques as in FIG. 7A. FIG. 7A shows a weld 68 joining the upper primer insert portion 56 and the lower primer insert portion 58. The weld 68 circumferentially surrounds the insert joint 60. FIG. 7B shows both a riveted and a coined method of joining the upper primer insert portion 56 and the lower primer insert portion 58. The lower primer insert portion 58 has a rivet 70 that extends through the upper primer insert portion 56 and secures the upper primer insert portion 56 and the lower primer insert portion 58. FIG. 7B also shows a coined method of joining the upper primer insert portion 56 and the lower primer insert portion 58. The lower primer insert portion 58 has a stud 72 that extends through the upper primer insert portion 56 and is coined 74 to secure the upper primer insert portion 56 and the lower primer insert portion 58. In addition, multiple methods may be used to increase the joint strength. The upper primer insert portion 56 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. The coupling element 30 extends with a taper to a smaller diameter at the tip 44. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 38 and extends through the bottom surface 34 into the propellant chamber 14. The coupling end 22 of the middle body extends the polymer through the primer flash hole 40 to form an aperture coating (not shown) while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14 to provide support and protection about the primer flash hole 40. When over-molded the coupling end 22 interlocks with the substantially cylindrical coupling element 30. The coupling element 30 extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 to the middle body component. The substantially cylindrical insert 32 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 28 and extends through the bottom surface 34 into the propellant chamber 14. The coupling end 22 extends the polymer through the primer flash hole 40 to form an aperture coating (not shown) while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14 to provide support and protection about the primer flash hole 40. When contacted the coupling end 22 interlocks with the substantially cylindrical coupling element 30, through the coupling element 30 that extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 and the middle body component 28.

FIGS. 8A-8C depict a side, cross-sectional view of a two piece primer insert having a tab and groove configuration used in a polymeric cartridge case. The substantially cylindrical primer insert 32 has an upper primer insert portion 56 and a lower primer insert portion 58 joined at insert joint 60. The insert joint 60 has a tab 62a and 62b that mate to the corresponding groove 64a and 64b to further secure the upper primer insert portion 56 and a lower primer insert portion 58. The location, shape and position of the tab 62a/62b and groove 64a/64b may be varied by the skilled artisan as necessary to secure the upper primer insert portion 56 and a lower primer insert portion 58. The upper primer insert portion 56 may be of the same or different materials than lower primer insert portion 58. The upper primer insert portion 56 mates to the lower primer insert portion 58 at insert joint 60 while retaining the primer flash hole 40 and the primer recess 38. The insert joint 60 may connect the upper primer insert portion 56 and the lower primer insert portion 58 by welding or bonding using solvent, adhesive, spin-welding, vibration-welding, ultrasonic-welding or laser-welding techniques. In addition, multiple methods may be used to increase the joint strength. The upper primer insert portion 56 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. The coupling element 30 extends with a taper to a smaller diameter at the tip 44. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 38 and extends through the bottom surface 34 into the propellant chamber 14. The coupling end 22 of the middle body extends the polymer through the primer flash hole 40 to form an aperture coating (not shown) while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14 to provide support and protection about the primer flash hole 40. When over-molded the coupling end 22 interlocks with the substantially cylindrical coupling element 30. The coupling element 30 extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 to the middle body component. The substantially cylindrical insert 32 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 28 and extends through the bottom surface 34 into the propellant chamber 14. The coupling end 22 extends the polymer through the primer flash hole 40 to form an aperture coating (not shown) while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14 to provide support and protection about the primer flash hole 40. When contacted the coupling end 22 interlocks with the substantially cylindrical coupling element 30, through the coupling element 30 that extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 and the middle body component 28.

Multiple piece inserts of the present invention may be configured in various ways. For example, the insert may be include three insert pieces, three insert pieces configured without the need for a diffuser, three insert pieces where one piece is a diffuser, three insert pieces where the diffuser is between the other insert pieces.

FIG. 9A depicts a side, cross-sectional view of a three piece primer insert having a tab and groove configuration used in a polymeric cartridge case. The substantially cylindrical primer insert 32 has an upper primer insert portion 56, a middle insert 76 and a lower primer insert portion 58 joined at the insert joints 60a and 60b. The middle insert 76 has tabs 62a and 62b that mate to the corresponding groove 64a and 64b to further secure the upper primer insert portion 56 and the middle insert 76. The middle insert 76 also has tabs 62c and 62d that mate to the corresponding groove 64c and 64d to further secure the lower primer insert portion 58 and the middle insert 76. This creates insert joint 60a between the upper primer insert portion 56 and the middle insert 76 and insert joint 60b between the lower primer insert portion 58 and the middle insert 76. The middle insert 76 has a flash hole aperture 78 that connects the upper primer insert portion 56 and the lower primer insert portion 58. In some instances the flash hole aperture 78 may have a diameter less than the diameter of the primer flash hole 40. The location, shape and position of the tab 62a-62d and groove 64a-64d may be varied by the skilled artisan as necessary to secure the upper primer insert portion 56, the middle insert 76 and the lower primer insert portion 58. The upper primer insert portion 56 may be of the same or different materials than lower primer insert portion 58. The upper primer insert portion 56 mates to the lower primer insert portion 58 at insert joint 60 while retaining the primer flash hole 40 and the primer recess 38. The insert joint 60 may connect the upper primer insert portion 56 and the lower primer insert portion 58 by welding or bonding using solvent, adhesive, spin-welding, vibration-welding, ultrasonic-welding or laser-welding techniques. In addition, multiple methods may be used to increase the joint strength. The upper primer insert portion 56 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. The coupling element 30 extends with a taper to a smaller diameter at the tip 44. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 38 and extends through the bottom surface 34 into the propellant chamber (not shown). The coupling end 22 of the middle body extends the polymer through the primer flash hole 40 to form an aperture coating (not shown) while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber (not shown) to provide support and protection about the primer flash hole 40. When over-molded the coupling end 22 interlocks with the substantially cylindrical coupling element 30. The coupling element 30 extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 to the middle body component. The substantially cylindrical insert 32 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 28 and extends through the bottom surface 34 into the propellant chamber (not shown). The coupling end 22 extends the polymer through the primer flash hole 40 to form an aperture coating (not shown) while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14 to provide support and protection about the primer flash hole 40. When contacted the coupling end 22 interlocks with the substantially cylindrical coupling element 30, through the coupling element 30 that extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 and the middle body component 28.

FIG. 9B depicts a side, cross-sectional view of a three piece primer insert having a tab and groove or a simple alignment configuration used in a polymeric cartridge case. The substantially cylindrical primer insert 32 has an upper primer insert portion 56, a middle insert 76 and a lower primer insert portion 58 joined at the insert joints 60a and 60b. The middle insert 76 has a tab aperture 80 that receives the tab 62 that mate to the corresponding groove 64 to further secure the upper primer insert portion 56, the middle insert 76 and the lower primer insert portion 58. Alternatively, the middle insert 76 may be a relative flat insert that aligns with the upper primer insert portion 56 and the lower primer insert portion 58. This creates insert joint 60a between the upper primer insert portion 56 and the middle insert 76 and insert joint 60b between the lower primer insert portion 58 and the middle insert 76. The middle insert 76 has a flash hole aperture 78 that connects the upper primer insert portion 56 and the lower primer insert portion 58. In some instances, the flash hole aperture 78 may have a diameter less than the diameter of the primer flash hole 40. The location, shape and position of the tab 62 and groove 64 may be varied by the skilled artisan as necessary to secure the upper primer insert portion 56, the middle insert 76 and the lower primer insert portion 58. The upper primer insert portion 56, the middle insert 76 and the lower primer insert portion 58 may individually be of the same or different materials. The upper primer insert portion 56 mates to the middle insert 76 at insert joint 60a and to the lower primer insert portion 58 at insert joint 60b while retaining the primer flash hole 40 and the primer recess 38. The inserts joint 60a and 60b may connect the upper primer insert portion 56, the middle insert 76 and the lower primer insert portion 58 by threading, riveting, locking, friction fitting, coining, snap fitting, chemical bonding, chemical welding, soldering, smelting, sintering, adhesive bonding, laser welding, ultrasonic welding, friction spot welding, friction stir welding spin-welding, vibration-welding, ultrasonic-welding or laser-welding techniques. In addition, multiple methods may be used to increase the joint strength.

The upper primer insert portion 56 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. The coupling element 30 extends with a taper to a smaller diameter at the tip 44. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 38 and extends through the bottom surface 34 into the propellant chamber (not shown). The coupling end 22 of the middle body extends the polymer through the primer flash hole 40 to form an aperture coating (not shown) while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14 to provide support and protection about the primer flash hole 40. When over-molded the coupling end 22 interlocks with the substantially cylindrical coupling element 30. The coupling element 30 extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 to the middle body component. The substantially cylindrical insert 32 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface 36. Located in the top surface 36 is a primer recess 38 that extends toward the bottom surface 34. A primer flash hole 40 is located in the primer recess 28 and extends through the bottom surface 34 into the propellant chamber 14. The coupling end 22 extends the polymer through the primer flash hole 40 to form an aperture coating (not shown) while retaining a passage from the top surface 36 through the bottom surface 34 and into the propellant chamber 14 to provide support and protection about the primer flash hole 40. When contacted the coupling end 22 interlocks with the substantially cylindrical coupling element 30, through the coupling element 30 that extends with a taper to a smaller diameter at the tip 44 to physical interlock the substantially cylindrical insert 32 and the middle body component 28.

FIG. 10 depicts a perspective view of a two piece primer insert used in a polymeric cartridge case. The substantially cylindrical primer insert 32 has an upper primer insert portion 56 and a lower primer insert portion 58 joined at insert joint 60. The upper primer insert portion 56 may be of the same or different materials than lower primer insert portion 58. The upper primer insert portion 56 mates to the lower primer insert portion 58 at insert joint 60 while retaining the primer flash hole 40 and the primer recess (not shown). The insert joint 60 may connect the upper primer insert portion 56 and the lower primer insert portion 58 by welding or bonding using solvent, adhesive, spin-welding, vibration-welding, ultrasonic-welding or laser-welding techniques. In addition, multiple methods may be used to increase the joint strength. The upper primer insert portion 56 includes a substantially cylindrical coupling element 30 extending from a bottom surface (not shown) that is opposite a top surface (not shown). The coupling element 30 extends with a taper to a smaller diameter at the tip 44. Located in the top surface (not shown) is a primer recess (not shown) that extends toward the bottom surface (not shown). A primer flash hole (not shown) is located in the primer recess (not shown) and extends through the bottom surface (not shown) into the propellant chamber (not shown). The lower primer insert portion 58 includes a flange 46 that may have a smooth transition around the surface or may have various designs positioned around the surface. The design, shape and number of notches 66 will depend on the specific application and desire of the manufacturer but may include 1, 2, 3, 4, 5 6, 7, 8, 9, 10, or more notches.

Chemical welding and chemical bonding involves the use of chemical compositions that undergoes a chemical or physical reaction resulting in the joining of the materials and the formation of a unitary primer insert. The chemicals may join the surfaces through the formation of a layer that contacts both surfaces or by melting the surfaces to a single interface between the surfaces.

Adhesive bonding involves the use of a polymeric adhesive, which undergoes a chemical or physical reaction, for eventual joint formation. The upper primer insert portion mates to the lower primer insert portion at the insert joint to which an adhesive material has been added to form a unitary primer insert. The adhesive includes high-strength and tough adhesives that can withstand both static and alternating loads.

Sintering involves the process of compacting and forming a solid mass of material by heat and/or pressure without melting it to the point of liquefaction. Materials that are identical or similar may be sintered in the temperature range for the specific time, e.g., stainless steel may be heated for 30-60 minutes at a temperature of between 2000-2350° F. However, materials that are dissimilar may be heated at the within the common temperature range (±400° F.) for the specific time (±0.5-2 hours). For example, the upper primer insert portion may be stainless steel with a temperature range form 2000-2350° F. for 30-60 minutes and the lower primer insert portion may be nickel 1850-2100° F. for 30-45 minutes (and vice versa) to allow the sintering at between 2000-2100° F. for 30-60 minutes. Similarly, the upper primer insert portion may be stainless steel with a temperature range form 2000-2350° F. for 30-60 minutes and the lower primer insert portion may be tungsten carbide 2600-2700° F. for 20-30 minutes to allow the sintering at between 2300-2600° F. for 30-60 minutes or longer if necessary. The skilled artisan readily understands the parameters associated with sintering materials of similar and different compositions and therefor there is no need in reciting all of the various combinations that can be formed in this application.

Welding techniques including laser welding, ultrasonic welding, friction spot welding, and friction stir welding. The welding methods can use the existing materials to fill in the insert joint or an additional material may be used to fill in the insert joint. The dissimilar multi-metal welded unitary primer insert must be examined to determine the crack sensitivity, ductility, susceptibility to corrosion, etc. In some cases, it is necessary to use a third metal that is soluble with each metal in order to produce a successful joint.

The two piece primer insert used in polymeric cartridge cases includes an upper primer insert portion and a lower primer insert portion joined at insert joint. The individual upper primer insert portion and lower primer insert portion may be formed in various methods. For example the individual upper primer insert portion and lower primer insert portion may be formed by metal injection molding, polymer injection molding, stamping, milling, molding, machining, punching, fine blanking, smelting, or any other method that will form insert portions that may be joined together to form a primer insert.

The two piece primer insert includes an individual upper primer insert portion and lower primer insert portion formed in various methods. For example, the individual upper primer insert portion and lower primer insert portion may be formed by stamping, milling, or machining and then joined together to form a primer insert.

For example, the individual upper primer insert portion, the lower primer insert portion or both may be formed by fineblanking. Fineblanking is a specialty type of metal stamping that can achieve part characteristics such as flatness and a full sheared edge to a degree that is nearly impossible using a conventional metal cutting or punching process and is used to achieve flatness and cut edge characteristics that are unobtainable by conventional stamping and punching methods. When the punch makes contact with the sheet, the metal begins to deform and bulge around the point of the punch. As the yield strength of the part material is exceeded by the downward force of the press, the point of the punch begins to penetrate the metal's surface. Both the punch and matrix, or button, begin to cut from their respective sides. When the ultimate tensile strength has been reached, the metal breaks or fractures from the edge of the punch to the edge of the matrix. This results in a cut edge that appears to be partially cut and partially broken or fractured. This cut edge condition often is referred to as the “cut band.” In most cases, the cut edge has about 10 percent to 30 percent of shear, and the remainder is fractured. The fracture has two primary causes. The distance between the punch and the matrix creates a leverage action and tends to pull the metal apart, causing it to rupture. The deformation that is allowed during the cutting process also allows the metal to fracture prematurely. Allowing the metal to deform severely during the cutting process results in straining of the metal, which in turn causes a stress. Trapped stresses in a product cause it to lose its flatness, which is why it is very difficult to maintain a critical flatness characteristic using conventional methods. Fineblanking requires the use of three very high-pressure pads in a special press. These pads hold the metal flat during the cutting process and keep the metal from plastically deforming during punch entry. Most fineblanking operations incorporate a V-ring into one of the high-pressure pads. This ring also is commonly referred to as a “stinger” or “impingement” ring. Before the punch contacts the part, the ring impales the metal, surrounds the perimeter of the part, and traps the metal from moving outward while pushing it inward toward the punch. This reduces rollover at the cut edge. Fineblanking operations usually require clearances of less than 0.0005 inch per side. This small clearance, combined with high pressure, results in a fully sheared part edge. Fineblanking is much like a cold extruding process. The slug (or part) is pushed or extruded out of the strip while it is held very tightly between the high-pressure holding plates and pads. The tight hold of the high-pressure plates prevents the metal from bulging or plastically deforming during the extrusion process.

The two piece primer insert includes an individual upper primer insert portion and lower primer insert portion formed in various methods. For example, the individual upper primer insert portion and lower primer insert portion may be formed by molding, injection molding or metal injection molding and then joined together to form a primer insert.

For example, when the individual upper primer insert portion and lower primer insert portion or both are metal injection molded, the raw materials are metal powders and a thermoplastic binder. There are at least two Binders included in the blend, a primary binder and a secondary binder. This blended powder mix is worked into the plasticized binder at elevated temperature in a kneader or shear roll extruder. The intermediate product is the so-called feedstock. It is usually granulated with granule sizes of several millimeters. In metal injection molding, only the binders are heated up, and that is how the metal is carried into the mold cavity.

In preparing a feedstock, it is important first to measure the actual density of each lot of both the metal powders and binders. This is extremely important especially for the metal powders in that each lot will be different based on the actual chemistry of that grade of powder. For example, 316L is comprised of several elements, such as Fe, Cr, Ni, Cu, Mo, P, Si, S and C. In order to be rightfully called a 316L, each of these elements must meet a minimum and maximum percentage weight requirement as called out in the relevant specification. Tables I-IV below provide other examples of the elemental compositions of some of the metal powders, feed stocks, metals, alloys and compositions of the present invention. Hence the variation in the chemistry within the specification results in a significant density variation within the acceptable composition range. Depending on the lot received from the powder producer, the density will vary depending on the actual chemistry received.

TABLE I Material Chemical Composition, Designation % - Low-Alloy Steels Code Fe Ni Mo C Si (max) MIM-2200(1) Bal. 1.5-2.5 0.5 max 0.1 max 1.0 MIM-2700 Bal. 6.5-8.5 0.5 max 0.1 max 1.0 MIM-4605(2) Bal. 1.5-2.5 0.2-0.5 0.4-0.6 1.0

TABLE II Material Designation Chemical Composition, % - Stainless Steels Code Fe Ni Cr Mo C Cu Nb + Ta Mn (max) Si (max) MIM-316L Bal. 10-14 16-18 2-3 0.03 max 2.0 1.0 MIM-420 Bal. 12-14 0.15-0.4 1.0 1.0 MIM-430L Bal. 16-18 0.05 max 1.0 1.0 MIM-17-4 PH Bal. 3-5 15.5-17.5 0.07 max 3-5 0.15-0.45 1.0 1.0

TABLE III Material Designation Chemical Composition, % - Soft-Magnetic Alloys Code Fe Ni Cr Co Si C (max) Mn V MIM-2200 Bal. 1.5-2.5 1.0 max 0.1 MIM-Fe—3%Si Bal. 2.5-3.5 0.05 MIM-Fe50%Ni Bal. 49-51 1.0 max 0.05 MIM-Fe50%Co Bal. 48-50 1.0 max 0.05 2.5 max MIM-430L Bal. 16-18 1.0 max 0.05 1.0 max

TABLE IV Nominal Chemical Composition, % - Controlled-Expansion Alloys Material Mn Si C Al Mg Zr Ti Cu Cr Mo Designation Fe Ni Co max max max max max max max max max max MIM-F15 Bal. 29 17 0.50 0.20 0.04 0.10 0.10 0.10 0.10 0.20 0.20 0.20

In addition to the specific compositions listed herein, the skill artisan recognizes the elemental composition of common commercial designations used by feedstock manufacturers and processors, e.g., C-0000 Copper and Copper Alloys; CFTG-3806-K Diluted Bronze Bearings; CNZ-1818 Copper and Copper Alloys; CNZP-1816 Copper and Copper Alloys; CT-1000 Copper and Copper Alloys; CT-1000-K Bronze Bearings; CTG-1001-K Bronze Bearings; CTG-1004-K Bronze Bearings; CZ-1000 Copper and Copper Alloys; CZ-2000 Copper and Copper Alloys; CZ-3000 Copper and Copper Alloys; CZP-1002 Copper and Copper Alloys; CZP-2002 Copper and Copper Alloys; CZP-3002 Copper and Copper Alloys; F-0000 Iron and Carbon Steel; F-0000-K Iron and Iron-Carbon Bearings; F-0005 Iron and Carbon Steel; F-0005-K Iron and Iron-Carbon Bearings; F-0008 Iron and Carbon Steel; F-0008-K Iron and Iron-Carbon Bearings; FC-0200 Iron-Copper and Copper Steel; FC-0200-K Iron-Copper Bearings; FC-0205 Iron-Copper and Copper Steel; FC-0205-K Iron-Copper-Carbon Bearings; FC-0208 Iron-Copper and Copper Steel; FC-0208-K Iron-Copper-Carbon Bearings; FC-0505 Iron-Copper and Copper Steel; FC-0508 Iron-Copper and Copper Steel; FC-0508-K Iron-Copper-Carbon Bearings; FC-0808 Iron-Copper and Copper Steel; FC-1000 Iron-Copper and Copper Steel; FC-1000-K Iron-Copper Bearings; FC-2000-K Iron-Copper Bearings; FC-2008-K Iron-Copper-Carbon Bearings; FCTG-3604-K Diluted Bronze Bearings; FD-0200 Diffusion-Alloyed Steel; FD-0205 Diffusion-Alloyed Steel; FD-0208 Diffusion-Alloyed Steel; FD-0400 Diffusion-Alloyed Steel; FD-0405 Diffusion-Alloyed Steel; FD-0408 Diffusion-Alloyed Steel; FF-0000 Soft-Magnetic Alloys; FG-0303-K Iron-Graphite Bearings; FG-0308-K Iron-Graphite Bearings; FL-4005 Prealloyed Steel; FL-4205 Prealloyed Steel; FL-4400 Prealloyed Steel; FL-4405 Prealloyed Steel; FL-4605 Prealloyed Steel; FL-4805 Prealloyed Steel; FL-48105 Prealloyed Steel; FL-4905 Prealloyed Steel; FL-5208 Prealloyed Steel; FL-5305 Prealloyed Steel; FLC-4608 Sinter-Hardened Steel; FLC-4805 Sinter-Hardened Steel; FLC-48108 Sinter-Hardened Steel; FLC-4908 Sinter-Hardened Steel; FLC2-4808 Sinter-Hardened Steel; FLDN2-4908 Diffusion-Alloyed Steel; FLDN4C2-4905 Diffusion-Alloyed Steel; FLN-4205 Hybrid Low-Alloy Steel; FLN-48108 Sinter-Hardened Steel; FLN2-4400 Hybrid Low-Alloy Steel; FLN2-4405 Hybrid Low-Alloy Steel; FLN2-4408 Sinter-Hardened Steel; FLN2C-4005 Hybrid Low-Alloy Steel; FLN4-4400 Hybrid Low-Alloy Steel; FLN4-4405 Hybrid Low-Alloy Steel; FLN4-4408 Sinter Hardened Steel; FLN4C-4005 Hybrid Low-Alloy Steel; FLN6-4405 Hybrid Low-Alloy Steel; FLN6-4408 Sinter-Hardened Steel; FLNC-4405 Hybrid Low-Alloy Steel; FLNC-4408 Sinter-Hardened Steel; FN-0200 Iron-Nickel and Nickel Steel; FN-0205 Iron-Nickel and Nickel Steel; FN-0208 Iron-Nickel and Nickel Steel; FN-0405 Iron-Nickel and Nickel Steel; FN-0408 Iron-Nickel and Nickel Steel; FN-5000 Soft-Magnetic Alloys; FS-0300 Soft-Magnetic Alloys; FX-1000 Copper-Infiltrated Iron and Steel; FX-1005 Copper-Infiltrated Iron and Steel; FX-1008 Copper-Infiltrated Iron and Steel; FX-2000 Copper-Infiltrated Iron and Steel; FX-2005 Copper-Infiltrated Iron and Steel; FX-2008 Copper-Infiltrated Iron and Steel; FY-4500 Soft-Magnetic Alloys; FY-8000 Soft-Magnetic Alloys; P/F-1020 Carbon Steel PF; P/F-1040 Carbon Steel PF; P/F-1060 Carbon Steel PF; P/F-10C40 Copper Steel PF; P/F-10050 Copper Steel PF; P/F-10060 Copper Steel PF; P/F-1140 Carbon Steel PF; P/F-1160 Carbon Steel PF; P/F-11C40 Copper Steel PF; P/F-11050 Copper Steel PF; P/F-11060 Copper Steel PF; P/F-4220 Low-Alloy P/F-42XX Steel PF; P/F-4240 Low-Alloy P/F-42XX Steel PF; P/F-4260 Low-Alloy P/F-42XX Steel PF; P/F-4620 Low-Alloy P/F-46XX Steel PF; P/F-4640 Low-Alloy P/F-46XX Steel PF; P/F-4660 Low-Alloy P/F-46XX Steel PF; P/F-4680 Low-Alloy P/F-46XX Steel PF; SS-303L Stainless Steel-300 Series Alloy; SS-303N1 Stainless Steel-300 Series Alloy; SS-303N2 Stainless Steel-300 Series Alloy; SS-304H Stainless Steel-300 Series Alloy; SS-304L Stainless Steel-300 Series Alloy; SS-304N1 Stainless Steel-300 Series Alloy; SS-304N2 Stainless Steel-300 Series Alloy; SS-316H Stainless Steel-300 Series Alloy; SS-316L Stainless Steel-300 Series Alloy; SS-316N1 Stainless Steel-300 Series Alloy; SS-316N2 Stainless Steel-300 Series Alloy; SS-409L Stainless Steel-400 Series Alloy; SS-409LE Stainless Steel-400 Series Alloy; SS-410 Stainless Steel-400 Series Alloy; SS-410L Stainless Steel-400 Series Alloy; SS-430L Stainless Steel-400 Series Alloy; SS-430N2 Stainless Steel-400 Series Alloy; SS-434L Stainless Steel-400 Series Alloy; SS-434LCb Stainless Steel-400 Series Alloy; and SS-434N2 Stainless Steel-400 Series Alloy.

Parts are molded until they feel that the cavity has been filled. Both mold design factors such as runner and gate size, gate placement, venting and molding parameters set on the molding machine affect the molded part. A helium Pycnometer can determine if there are voids trapped inside the parts. During molding, you have a tool that can be used to measure the percent of theoretical density achieved on the “Green” or molded part. By crushing the measured “green” molded part back to powder, you can now confirm the percent of air (or voids) trapped in the molded part. To measure this, the density of the molded part should be measured in the helium Pycnometer and compared to the theoretical density of the feedstock. Then, take the same molded part that was used in the density test and crush it back to powder. If this granulate shows a density of more than 100% of that of the feedstock, then some of the primary binders have been lost during the molding process. The molding process needs to be corrected because using this process with a degraded feedstock will result in a larger shrinkage and result in a part smaller than that desired. It is vital to be sure that your molded parts are completely filled before continuing the manufacturing process for debinding and sintering. The helium Pycnometer provides this assurance. Primary debinding properly debound parts are extremely important to establish the correct sintering profile. The primary binder must be completely removed before attempting to start to remove the secondary binder as the secondary binder will travel through the pores created by the extraction of the primary binder. Primary debinding techniques depend on the feedstock type used to make the parts. However the feedstock supplier knows the amount of primary binders that have been added and should be removed before proceeding to the next process step. The feedstock supplier provides a minimum “brown density” that must be achieved before the parts can be moved into a furnace for final debinding and sintering. This minimum brown density will take into account that a small amount of the primary binder remnant may be present and could be removed by a suitable hold during secondary debinding and sintering. The sintering profile should be adjusted to remove the remaining small percent of primary binder before the removal of the secondary binder. Most external feedstock manufacturers provide only a weight loss percent that should be obtained to define suitable debinding. Solvent debound parts must be thoroughly dried, before the helium Pycnometer is used to determine the “brown” density so that the remnant solvent in the part does not affect the measured density value. When the feedstock manufacturer gives you the theoretical density of the “brown” or debound part, can validate the percent of debinding that has been achieved. Most Metal Injection Molding (MIM) operations today perform the secondary debinding and sintering in the same operation. Every MIM molder has gates and runners left over from molding their parts. So, you will be able to now re-use your gates and runners with confidence that they will shrink correctly after sintering. If the feedstock producers have given you the actual and theoretical densities of their feedstock, you can easily measure the densities of the gates and runners and compare the results to the values supplied. Once the regrind densities are higher than that required to maintain the part dimensions, the regrinds are no longer reusable.

Feedstock in accordance with the present invention may be prepared by blending the powdered metal with the binder and heating the blend to form a slurry. Uniform dispersion of the powdered metal in the slurry may be achieved by employing high shear mixing. The slurry may then be cooled to ambient temperature and then granulated to provide the feedstock for the metal injection molding.

One embodiment of the injection molded primer insert may include a composition where Ni may be 2.0, 2.25, 2.50, 2.75, 3.0, 3.25, 3.5, 3.75, 4.0, 4.25, 4.50, 4.75, 5.0, 5.25, 5.5, 5.75, 6.0, 6.25, 6.50, 6.75, 7.0, 7.25, 7.5, 7.75, 8.0, 8.25, 8.50, 8.75, 9.0, 9.25, 9.5, 9.75, 10.0, 10.25, 10.50, 10.75, 11.0, 11.25, 11.5, 11.75, 12.0, 12.25, 12.50, 12.75, 13.0, 13.25, 13.5, 13.75, 14.0, 14.25, 14.50, 14.75, 15.0, 15.25, 15.5, 15.75, 16.0, 16.25, 16.50, 16.75, or 17.0%; Cr may be 9.0, 9.25, 9.5, 9.75, 10.0, 10.25, 10.50, 10.75, 11.0, 11.25, 11.5, 11.75, 12.0, 12.25, 12.50, 12.75, 13.0, 13.25, 13.5, 13.75, 14.0, 14.25, 14.50, 14.75, 15.0, 15.25, 15.5, 15.75, 16.0, 16.25, 16.50, 16.75, 17.0, 17.25, 17.5, 17.75, 18.0, 18.25, 18.50, 18.75, 19.0, 19.25, 19.5, 19.75, or 20.0%; Mo may be 0.00, 0.025, 0.050, 0.075, 0.10, 0.125, 0.150, 0.175, 0.20, 0.225, 0.250, 0.275, 0.30, 0.325, 0.350, 0.375, 0.40, 0.425, 0.450, 0.475, 0.50, 0.525, 0.550, 0.575, 0.60, 0.625, 0.650, 0.675, 0.70, 0.725, 0.750, 0.775, 0.80, 0.825, 0.850, 0.875, 0.90, 0.925, 0.950, 1.0, 1.25, 1.5, 1.75, 2.0, 2.25, 2.50, 2.75, 3.0, 3.25, 3.5, 3.75, 4.0, 4.25, 4.50, 4.75, 5.0, 5.25, 5.5, 5.75, 6.0, 6.25, 6.50, 6.75, or 7.0%; C may be 0.00, 0.025, 0.050, 0.075, 0.10, 0.125, 0.150, 0.175, 0.20, 0.225, 0.250, 0.275, 0.30, 0.325, 0.350, 0.375, 0.40, 0.425, 0.450, 0.475, 0.50, 0.525, 0.550, 0.575, 0.60, 0.625, 0.650, 0.675, 0.70, 0.725, 0.750, 0.775, 0.80, 0.825, 0.850, 0.875, 0.90, 0.925, 0.950, or 1.00%; Cu may be 0.00, 0.025, 0.050, 0.075, 0.10, 0.125, 0.150, 0.175, 0.20, 0.225, 0.250, 0.275, 0.30, 0.325, 0.350, 0.375, 0.40, 0.425, 0.450, 0.475, 0.50, 0.525, 0.550, 0.575, 0.60, 0.625, 0.650, 0.675, 0.70, 0.725, 0.750, 0.775, 0.80, 0.825, 0.850, 0.875, 0.90, 0.925, 0.950, 1.0, 1.25, 1.5, 1.75, 2.0, 2.25, 2.50, 2.75, 3.0, 3.25, 3.5, 3.75, 4.0, 4.25, 4.50, 4.75, 5.0, 5.25, 5.5, 5.75, 6.0, 6.25, 6.50, 6.75, 7.0, 7.25, 7.5, 7.75, or 8.0%; Nb+Ta may be 0.00, 0.025, 0.050, 0.075, 0.10, 0.125, 0.150, 0.175, 0.20, 0.225, 0.250, 0.275, 0.30, 0.325, 0.350, 0.375, 0.40, 0.425, 0.450, 0.475, 0.50, 0.525, 0.550, 0.575, 0.60, 0.625, 0.650, 0.675, 0.70, 0.725, 0.750, 0.775, or 0.80%; Mn may be 0.00, 0.025, 0.050, 0.075, 0.10, 0.125, 0.150, 0.175, 0.20, 0.225, 0.250, 0.275, 0.30, 0.325, 0.350, 0.375, 0.40, 0.425, 0.450, 0.475, 0.50, 0.525, 0.550, 0.575, 0.60, 0.625, 0.650, 0.675, 0.70, 0.725, 0.750, 0.775, 0.80, 0.825, 0.850, 0.875, 0.90, 0.925, 0.950, 1.0, 1.25, 1.5, 1.75, 2.0, 2.25, 2.50, 2.75, 3.0, 3.25, 3.5, 3.75, 4.0, 4.25, 4.50, 4.75, 5.0, 5.25, 5.5, 5.75, or 6.0%; Si may be 0.00, 0.025, 0.050, 0.075, 0.10, 0.125, 0.150, 0.175, 0.20, 0.225, 0.250, 0.275, 0.30, 0.325, 0.350, 0.375, 0.40, 0.425, 0.450, 0.475, 0.50, 0.525, 0.550, 0.575, 0.60, 0.625, 0.650, 0.675, 0.70, 0.725, 0.750, 0.775, 0.80, 0.825, 0.850, 0.875, 0.90, 0.925, 0.950, 1.0, 1.25, 1.5, 1.75, 2.0, 2.25, 2.50, 2.75, 3.0, 3.25, 3.5, 3.75, or 4.0%; and the balance Fe. For example, one embodiment of the injection molded primer insert may include any amount in the range of 2-16% Ni; 10-20% Cr; 0-5% Mo; 0-0.6% C; 0-6.0% Cu; 0-0.5% Nb+Ta; 0-4.0% Mn; 0-2.0% Si and the balance Fe. One embodiment of the injection molded primer insert may include any amount in the range of 2-6% Ni; 13.5-19.5% Cr; 0-0.10% C; 1-7.0% Cu; 0.05-0.65% Nb+Ta; 0-3.0% Mn; 0-3.0% Si and the balance Fe. One embodiment of the injection molded primer insert may include any amount in the range of 3-5% Ni; 15.5-17.5% Cr; 0-0.07% C; 3-5.0% Cu; 0.15-0.45% Nb+Ta; 0-1.0% Mn; 0-1.0% Si and the balance Fe. One embodiment of the injection molded primer insert may include any amount in the range of 10-14% Ni; 16-18% Cr; 2-3% Mo; 0-0.03% C; 0-2% Mn; 0-1% Si and the balance Fe. One embodiment of the injection molded primer insert may include any amount in the range of 12-14% Cr; 0.15-0.4% C; 0-1% Mn; 0-1% Si and the balance Fe. One embodiment of the injection molded primer insert may include any amount in the range of 16-18% Cr; 0-0.05% C; 0-1% Mn; 0-1% Si and the balance Fe.

Titanium alloys that may be used in this invention include any alloy or modified alloy known to the skilled artisan including titanium grades 5-38 and more specifically titanium grades 5, 9, 18, 19, 20, 21, 23, 24, 25, 28, 29, 35, 36 or 38. Grades 5, 23, 24, 25, 29, 35, or 36 annealed or aged; Grades 9, 18, 28, or 38 cold-worked and stress-relieved or annealed; Grades 9, 18, 23, 28, or 29 transformed-beta condition; and Grades 19, 20, or 21 solution-treated or solution-treated and aged. Grade 5, also known as Ti6Al4V, Ti-6Al-4V or Ti 6-4, is the most commonly used alloy. It has a chemical composition of 6% aluminum, 4% vanadium, 0.25% (maximum) iron, 0.2% (maximum) oxygen, and the remainder titanium. It is significantly stronger than commercially pure titanium while having the same stiffness and thermal properties (excluding thermal conductivity, which is about 60% lower in Grade 5 Ti than in CP Ti); Grade 6 contains 5% aluminum and 2.5% tin. It is also known as Ti-5Al-2.5Sn. This alloy has good weldability, stability and strength at elevated temperatures; Grade 7 and 7Hcontains 0.12 to 0.25% palladium. This grade is similar to Grade 2. The small quantity of palladium added gives it enhanced crevice corrosion resistance at low temperatures and high pH; Grade 9 contains 3.0% aluminum and 2.5% vanadium. This grade is a compromise between the ease of welding and manufacturing of the “pure” grades and the high strength of Grade 5; Grade 11 contains 0.12 to 0.25% palladium; Grade 12 contains 0.3% molybdenum and 0.8% nickel; Grades 13, 14, and 15 all contain 0.5% nickel and 0.05% ruthenium; Grade 16 contains 0.04 to 0.08% palladium; Grade 16H contains 0.04 to 0.08% palladium; Grade 17 contains 0.04 to 0.08% palladium; Grade 18 contains 3% aluminum, 2.5% vanadium and 0.04 to 0.08% palladium; Grade 19 contains 3% aluminum, 8% vanadium, 6% chromium, 4% zirconium, and 4% molybdenum; Grade 20 contains 3% aluminum, 8% vanadium, 6% chromium, 4% zirconium, 4% molybdenum and 0.04% to 0.08% palladium; Grade 21 contains 15% molybdenum, 3% aluminum, 2.7% niobium, and 0.25% silicon; Grade 23 contains 6% aluminum, 4% vanadium, 0.13% (maximum) Oxygen; Grade 24 contains 6% aluminum, 4% vanadium and 0.04% to 0.08% palladium. Grade 25 contains 6% aluminum, 4% vanadium and 0.3% to 0.8% nickel and 0.04% to 0.08% palladium; Grades 26, 26H, and 27 all contain 0.08 to 0.14% ruthenium; Grade 28 contains 3% aluminum, 2.5% vanadium and 0.08 to 0.14% ruthenium; Grade 29 contains 6% aluminum, 4% vanadium and 0.08 to 0.14% ruthenium; Grades 30 and 31 contain 0.3% cobalt and 0.05% palladium; Grade 32 contains 5% aluminum, 1% tin, 1% zirconium, 1% vanadium, and 0.8% molybdenum; Grades 33 and 34 contain 0.4% nickel, 0.015% palladium, 0.025% ruthenium, and 0.15% chromium; Grade 35 contains 4.5% aluminum, 2% molybdenum, 1.6% vanadium, 0.5% iron, and 0.3% silicon; Grade 36 contains 45% niobium; Grade 37 contains 1.5% aluminum; and Grade 38 contains 4% aluminum, 2.5% vanadium, and 1.5% iron. Its mechanical properties are very similar to Grade 5, but has good cold workability similar to grade 9. One embodiment includes a Ti6Al4V composition. One embodiment includes a composition having 3-12% aluminum, 2-8% vanadium, 0.1-0.75% iron, 0.1-0.5% oxygen, and the remainder titanium. More specifically, about 6% aluminum, about 4% vanadium, about 0.25% iron, about 0.2% oxygen, and the remainder titanium. For example, one Ti composition may include 10 to 35% Cr, 0.05 to 15% Al, 0.05 to 2% Ti, 0.05 to 2% Y2O5, with the balance being either Fe, Ni or Co, or an alloy consisting of 20±1.0% Cr, 4.5±0.5% Al, 0.5±0.1% Y2O5 or ThO2, with the balance being Fe. For example, one Ti composition may include 15.0-23.0% Cr, 0.5-2.0% Si, 0.0-4.0% Mo, 0.0-1.2% Nb, 0.0-3.0% Fe, 0.0-0.5% Ti, 0.0-0.5% Al, 0.0-0.3% Mn, 0.0-0.1% Zr, 0.0-0.035% Ce, 0.005-0.025% Mg, 0.0005-0.005% B, 0.005-0.3% C, 0.0-20.0% Co, balance Ni. Sample Ti-based feedstock component includes 0-45% metal powder; 15-40% binder; 0-10% Polymer (e.g., thermoplastics and thermosets); surfactant 0-3%; lubricant 0-3%; sintering aid 0-1%. Another sample Ti-based feedstock component includes about 62% TiH2 powder as a metal powder; about 29% naphthalene as a binder; about 2.1-2.3% polymer (e.g., EVA/epoxy); about 2.3% SURFONIC N-100° as a Surfactant; lubricant is 1.5% stearic acid as a; about 0.4% silver as a sintering Aid. Examples of metal compounds include metal hydrides, such as TiH2, and intermetallics, such as TiAl and TiAl3. A specific instance of an alloy includes Ti-6Al,4V, among others. In another embodiment, the metal powder comprises at least approximately 45% of the volume of the feedstock, while in still another, it comprises between approximately 54.6% and 70.0%. In addition, Ti—Al alloys may consists essentially of 32-38% of Al and the balance of Ti and contains 0.005-0.20% of B, and the alloy which essentially consists of the above quantities of Al and Ti and contains, in addition to the above quantity of B, up to 0.2% of C, up to 0.3% of 0 and/or up to 0.3% of N (provided that 0+N add up to 0.4%) and c) 0.05-3.0% of Ni and/or 0.05-3.0% of Si, and the balance of Ti.

The amount of powdered metal and binder in the feedstock may be selected to optimize moldability while insuring acceptable green densities. In one embodiment, the feedstock used for the metal injection molding portion of the invention may include at least about 40 percent by weight powdered metal, in another about 50 percent by weight powdered metal or more. In one embodiment, the feedstock includes at least about 60 percent by weight powdered metal, preferably about 65 percent by weight or more powdered metal. In yet another embodiment, the feedstock includes at least about 75 percent by weight powdered metal. In yet another embodiment, the feedstock includes at least about 80 percent by weight powdered metal. In yet another embodiment, the feedstock includes at least about 85 percent by weight powdered metal. In yet another embodiment, the feedstock includes at least about 90 percent by weight powdered metal.

The binding agent may be any suitable binding agent that does not destroy or interfere with the powdered metals. The binder may be present in an amount of about 50 percent or less by weight of the feedstock. In one embodiment, the binder is present in an amount ranging from 10 percent to about 50 percent by weight. In another embodiment, the binder is present in an amount of about 25 percent to about 50 percent by weight of the feedstock. In another embodiment, the binder is present in an amount of about 30 percent to about 40 percent by weight of the feedstock. In one embodiment, the binder is an aqueous binder. In another embodiment, the binder is an organic-based binder. Examples of binders include, but are not limited to, thermoplastic resins, waxes, and combinations thereof. Non-limiting examples of thermoplastic resins include polyolefins such as acrylic polyethylene, polypropylene, polystyrene, polyvinyl chloride, polyethylene carbonate, polyethylene glycol, and mixtures thereof. Suitable waxes include, but are not limited to, microcrystalline wax, bee wax, synthetic wax, and combinations thereof.

Examples of suitable powdered metals for use in the feedstock include, but are not limited to: stainless steel including martensitic and austenitic stainless steel, steel alloys, tungsten alloys, soft magnetic alloys such as iron, iron-silicon, electrical steel, iron-nickel (50Ni-50F3), low thermal expansion alloys, or combinations thereof. In one embodiment, the powdered metal is a mixture of stainless steel, brass and tungsten alloy. The stainless steel used in the present invention may be any 1 series carbon steels, 2 series nickel steels, 3 series nickel-chromium steels, 4 series molybdenum steels, series chromium steels, 6 series chromium-vanadium steels, 7 series tungsten steels, 8 series nickel-chromium-molybdenum steels, or 9 series silicon-manganese steels, e.g., 102, 174, 201, 202, 300, 302, 303, 304, 308, 309, 316, 316L, 316Ti, 321, 405, 408, 409, 410, 416, 420, 430, 439, 440, 446 or 601-665 grade stainless steel.

As known to those of ordinary skill in the art, stainless steel is an alloy of iron and at least one other component that imparts corrosion resistance. As such, in one embodiment, the stainless steel is an alloy of iron and at least one of chromium, nickel, silicon, molybdenum, or mixtures thereof. Examples of such alloys include, but are not limited to, an alloy containing about 1.5 to about 2.5 percent nickel, no more than about 0.5 percent molybdenum, no more than about 0.15 percent carbon, and the balance iron with a density ranging from about 7 g/cm3 to about 8 g/cm3; an alloy containing about 6 to about 8 percent nickel, no more than about 0.5 percent molybdenum, no more than about 0.15 percent carbon, and the balance iron with a density ranging from about 7 g/cm3 to about 8 g/cm3; an alloy containing about 0.5 to about 1 percent chromium, about 0.5 percent to about 1 percent nickel, no more than about 0.5 percent molybdenum, no more than about 0.2 percent carbon, and the balance iron with a density ranging from about 7 g/cm3 to about 8 g/cm3; an alloy containing about 2 to about 3 percent nickel, no more than about 0.5 percent molybdenum, about 0.3 to about 0.6 percent carbon, and the balance iron with a density ranging from about 7 g/cm3 to about 8 g/cm3; an alloy containing about 6 to about 8 percent nickel, no more than about 0.5 percent molybdenum, about 0.2 to about 0.5 percent carbon, and the balance iron with a density ranging from about 7 g/cm3 to about 8 g/cm3; an alloy containing about 1 to about 1.6 percent chromium, about 0.5 percent or less nickel, no more than about 0.5 percent molybdenum, about 0.9 to about 1.2 percent carbon, and the balance iron with a density ranging from about 7 g/cm3 to about 8 g/cm3; and combinations thereof.

Suitable tungsten alloys include an alloy containing about 2.5 to about 3.5 percent nickel, about 0.5 percent to about 2.5 percent copper or iron, and the balance tungsten with a density ranging from about 17.5 g/cm3 to about 18.5 g/cm3; about 3 to about 4 percent nickel, about 94 percent tungsten, and the balance copper or iron with a density ranging from about 17.5 g/cm3 to about 18.5 g/cm3; and mixtures thereof.

In addition, the binders may contain additives such as antioxidants, coupling agents, surfactants, elasticizing agents, dispersants, and lubricants as disclosed in U.S. Pat. No. 5,950,063, which is hereby incorporated by reference in its entirety. Suitable examples of antioxidants include, but are not limited to thermal stabilizers, metal deactivators, or combinations thereof. In one embodiment, the binder includes about 0.1 to about 2.5 percent by weight of the binder of an antioxidant. Coupling agents may include but are not limited to titanate, aluminate, silane, or combinations thereof. Typical levels range between 0.5 and 15% by weight of the binder.

The polymeric and composite casing components may be injection molded. Polymeric materials for the bullet-end and middle body components must have propellant compatibility and resistance to gun cleaning solvents and grease, as well as resistance to chemical, biological and radiological agents. The polymeric materials must have a temperature resistance higher than the cook-off temperature of the propellant, typically about 320° F. The polymeric materials must have elongation-to-break values that to resist deformation under interior ballistic pressure as high as 60,000 psi in all environments (temperatures from about −65 to about 320° F. and humidity from 0 to 100% relative humidity). According to one embodiment, the middle body component is either molded onto or snap-fit to the casing head-end component after which the bullet-end component is snap-fit or interference fit to the middle body component. The components may be formed from high-strength polymer, composite or ceramic.

Examples of suitable high strength polymers include composite polymer material including a tungsten metal powder, nylon 6/6, nylon 6, and glass fibers; and a specific gravity in a range of 3-10. The tungsten metal powder may be 50%-96% of a weight of the bullet body. The polymer material also includes about 0.5-15%, preferably about 1-12%, and most preferably about 2-9% by weight, of nylon 6/6, about 0.5-15%, preferably about 1-12%, and most preferably about 2-9% by weight, of nylon 6, and about 0.5-15%, preferably about 1-12%, and most preferably about 2-9% by weight, of glass fibers. It is most suitable that each of these ingredients be included in amounts less than 10% by weight. The cartridge casing body may be made of a modified ZYTEL® resin, available from E.I. DuPont De Nemours Co., a modified 612 nylon resin, modified to increase elastic response.

Examples of suitable polymers include polyurethane prepolymer, cellulose, fluoro-polymer, ethylene inter-polymer alloy elastomer, ethylene vinyl acetate, nylon, polyether imide, polyester elastomer, polyester sulfone, polyphenyl amide, polypropylene, polyvinylidene fluoride or thermoset polyurea elastomer, acrylics, homopolymers, acetates, copolymers, acrylonitrile-butadinen-styrene, thermoplastic fluoro polymers, inomers, polyamides, polyamide-imides, polyacrylates, polyatherketones, polyaryl-sulfones, polybenzimidazoles, polycarbonates, polybutylene, terephthalates, polyether imides, polyether sulfones, thermoplastic polyimides, thermoplastic polyurethanes, polyphenylene sulfides, polyethylene, polypropylene, polysulfones, polyvinylchlorides, styrene acrylonitriles, polystyrenes, polyphenylene, ether blends, styrene maleic anhydrides, polycarbonates, allyls, aminos, cyanates, epoxies, phenolics, unsaturated polyesters, bismaleimides, polyurethanes, silicones, vinylesters, or urethane hybrids. Examples of suitable polymers also include aliphatic or aromatic polyamide, polyeitherimide, polysulfone, polyphenylsulfone, poly-phenylene oxide, liquid crystalline polymer and polyketone. Examples of suitable composites include polymers such as polyphenylsulfone reinforced with between about 30 and about 70 weight percent, and preferably up to about 65 weight percent of one or more reinforcing materials selected from glass fiber, ceramic fiber, carbon fiber, mineral fillers, organo nanoclay, or carbon nanotube. Preferred reinforcing materials, such as chopped surface-treated E-glass fibers provide flow characteristics at the above-described loadings comparable to unfilled polymers to provide a desirable combination of strength and flow characteristics that permit the molding of head-end components. Composite components can be formed by machining or injection molding. Finally, the cartridge case must retain sufficient joint strength at cook-off temperatures. More specifically, polymers suitable for molding of the projectile-end component have one or more of the following properties: Yield or tensile strength at −65° F.>10,000 psi Elongation-to-break at −65° F.>15% Yield or tensile strength at 73° F.>8,000 psi Elongation-to-break at 73° F.>50% Yield or tensile strength at 320° F.>4,000 psi Elongation-to-break at 320° F.>80%. Polymers suitable for molding of the middle-body component have one or more of the following properties: Yield or tensile strength at −65° F.>10,000 psi Yield or tensile strength at 73° F.>8,000 psi Yield or tensile strength at 320° F.>4,000 psi.

Commercially available polymers suitable for use in the present invention thus include polyphenylsulfones; copolymers of polyphenylsulfones with polyether-sulfones or polysulfones; copolymers and blends of polyphenylsulfones with polysiloxanes; poly(etherimide-siloxane); copolymers and blends of polyetherimides and polysiloxanes, and blends of polyetherimides and poly(etherimide-siloxane) copolymers; and the like. Particularly preferred are polyphenylsulfones and their copolymers with poly-sulfones or polysiloxane that have high tensile strength and elongation-to-break to sustain the deformation under high interior ballistic pressure. Such polymers are commercially available, for example, RADEL® R5800 polyphenylesulfone from Solvay Advanced Polymers. The polymer can be formulated with up to about 10 wt % of one or more additives selected from internal mold release agents, heat stabilizers, anti-static agents, colorants, impact modifiers and UV stabilizers.

The polymers of the present invention can also be used for conventional two-piece metal-plastic hybrid cartridge case designs and conventional shotgun shell designs. One example of such a design is an ammunition cartridge with a one-piece substantially cylindrical polymeric cartridge casing body with an open projectile-end and an end opposing the projectile-end with a male or female coupling element; and a cylindrical metal cartridge casing head-end component with an essentially closed base end with a primer hole opposite an open end having a coupling element that is a mate for the coupling element on the opposing end of the polymeric cartridge casing body joining the open end of the head-end component to the opposing end of the polymeric cartridge casing body. The high polymer ductility permits the casing to resist breakage.

One embodiment includes a 2 cavity prototype mold having an upper portion and a base portion for a 5.56 case having a metal insert over-molded with a Nylon 6 (polymer) based material. In this embodiment the polymer in the base includes a lip or flange to extract the case from the weapon. One 2-cavity prototype mold to produce the upper portion of the 5.56 case can be made using a stripper plate tool using an Osco hot spur and two subgates per cavity. Another embodiment includes a subsonic version, the difference from the standard and the subsonic version is the walls are thicker thus requiring less powder. This will decrease the velocity of the bullet thus creating a subsonic round.

The extracting inserts is used to give the polymer case a tough enough ridge and groove for the weapons extractor to grab and pull the case out the chamber of the gun. The extracting insert is made of 17-4 stainless steel that is hardened to 42-45rc. The insert may be made of aluminum, brass, cooper, steel or even an engineered resin with enough tensile strength.

The insert is over molded in an injection molded process using a nano clay particle filled Nylon material. The inserts can be machined or stamped. In addition, an engineered resin able to withstand the demand on the insert allows injection molded and/or even transfer molded.

One of ordinary skill in the art will know that many propellant types and weights can be used to prepare workable ammunition and that such loads may be determined by a careful trial including initial low quantity loading of a given propellant and the well known stepwise increasing of a given propellant loading until a maximum acceptable load is achieved. Extreme care and caution is advised in evaluating new loads. The propellants available have various burn rates and must be carefully chosen so that a safe load is devised.

The components may be made of polymeric compositions, metals, ceramics, alloys, or combinations and mixtures thereof. In addition, the components may be mixed and matched with one or more components being made of different materials. For example, the middle body component (not shown) may be polymeric; the bullet-end component 18 may be polymeric; and a substantially cylindrical insert (not shown) may be metal. Similarly, the middle body component (not shown) may be polymeric; the bullet-end component 18 may be metal; and a substantially cylindrical insert (not shown) may be an alloy. The middle body component (not shown) may be polymeric; the bullet-end component 18 may be an alloy; and a substantially cylindrical insert (not shown) may be an alloy. The middle body component (not shown); the bullet-end component 18; and/or the substantially cylindrical insert may be made of a metal that is formed by a metal injection molding process.

The molded substantially cylindrical insert 32 is then bound to the middle body component 28. In the metal injection molding process of making the substantially cylindrical insert 32 a mold is made in the shape of the substantially cylindrical insert 32 including the desired profile of the primer recess (not shown). The substantially cylindrical insert 32 includes a substantially cylindrical coupling element 30 extending from a bottom surface 34 that is opposite a top surface (not shown). Located in the top surface (not shown) is a primer recess (not shown) that extends toward the bottom surface 34. A primer flash hole (not shown). is located in the substantially cylindrical insert 32 and extends through the bottom surface 34 into the powder chamber 14. The coupling end (not shown) extends through the primer flash hole (not shown) to form an aperture coating (not shown) while retaining a passage from the top surface (not shown) through the bottom surface (not shown) and into the powder chamber 14 to provides support and protection about the primer flash hole (not shown). When contacted the coupling end (not shown) interlocks with the substantially cylindrical coupling element 30, through the coupling element 30 that extends with a taper to a smaller diameter at the tip (not shown) to form a physical interlock between substantially cylindrical insert 32 and middle body component 28.

For example, the metal injection molding process, which generally involves mixing fine metal powders with binders to form a feedstock that is injection molded into a closed mold, may be used to form a substantially cylindrical insert. After ejection from the mold, the binders are chemically or thermally removed from the substantially cylindrical insert so that the part can be sintered to high density. During the sintering process, the individual metal particles metallurgically bond together as material diffusion occurs to remove most of the porosity left by the removal of the binder.

The raw materials for metal injection molding are metal powders and a thermoplastic binder. There are at least two Binders included in the blend, a primary binder and a secondary binder. This blended powder mix is worked into the plasticized binder at elevated temperature in a kneader or shear roll extruder. The intermediate product is the so-called feedstock. It is usually granulated with granule sizes of several millimeters. In metal injection molding, only the binders are heated up, and that is how the metal is carried into the mold cavity.

The two piece primer insert includes an individual upper primer insert portion and lower primer insert portion formed in various methods. For example, the individual upper primer insert portion may be formed by metal injection molding, polymer injection molding, stamping, milling, molding, machining, punching, fine blanking, smelting, or any other method. The lower primer insert portion may be formed by metal injection molding, polymer injection molding, stamping, milling, molding, machining, punching, fine blanking, smelting, or any other method that will form insert portions.

The individual upper primer insert portion may be formed from any material, any metal, any alloy, any plastic, any polymer or any composition known to the skilled artisan or listed herein. The individual lower primer insert portion may be formed from any material, any metal, any alloy, any plastic, any polymer or any composition known to the skilled artisan or listed herein.

The individual upper primer insert portion may be formed from entirely or in part from a copolymer of polylactic acid and polycarbonate, the concentration polylactic acid may be between 5-97% and the polycarbonate may be between 5-97%. The 5-97% is meant to be inclusive and include all percentages between 5 and 97 including fractional increments thereof, e.g., 5, 5.25, 5.5, 6, 6.75, 7, 7.4, 8, 8.9, 9, 10 15, 20, 25, 30, 35, 40, 45, 50, 55, 60, 65, 70, 75, 80, 85, 90, 95, or 97. In addition, the copolymer may include other polymers, additives, fibers, nanoclay, metals etc. When other polymers are present the combined percentage of polylactic acid and polycarbonate may be 5, 6, 7, 8, 9, 10 15, 20, 25, 30, 35, 40, 45, 50, 55, 60, 65, 70, 75, 80, 85, 90, 95, or 100.

The description of the preferred embodiments should be taken as illustrating, rather than as limiting, the present invention as defined by the claims. As will be readily appreciated, numerous combinations of the features set forth above can be utilized without departing from the present invention as set forth in the claims. Such variations are not regarded as a departure from the spirit and scope of the invention, and all such modifications are intended to be included within the scope of the following claims.

It is contemplated that any embodiment discussed in this specification can be implemented with respect to any method, kit, reagent, or composition of the invention, and vice versa. Furthermore, compositions of the invention can be used to achieve methods of the invention.

It will be understood that particular embodiments described herein are shown by way of illustration and not as limitations of the invention. The principal features of this invention can be employed in various embodiments without departing from the scope of the invention. Those skilled in the art will recognize, or be able to ascertain using no more than routine experimentation, numerous equivalents to the specific procedures described herein. Such equivalents are considered to be within the scope of this invention and are covered by the claims.

All publications and patent applications mentioned in the specification are indicative of the level of skill of those skilled in the art to which this invention pertains. All publications and patent applications are herein incorporated by reference to the same extent as if each individual publication or patent application was specifically and individually indicated to be incorporated by reference.

The use of the word “a” or “an” when used in conjunction with the term “comprising” in the claims and/or the specification may mean “one,” but it is also consistent with the meaning of “one or more,” “at least one,” and “one or more than one.” The use of the term “or” in the claims is used to mean “and/or” unless explicitly indicated to refer to alternatives only or the alternatives are mutually exclusive, although the disclosure supports a definition that refers to only alternatives and “and/or.” Throughout this application, the term “about” is used to indicate that a value includes the inherent variation of error for the device, the method being employed to determine the value, or the variation that exists among the study subjects.

As used in this specification and claim(s), the words “comprising” (and any form of comprising, such as “comprise” and “comprises”), “having” (and any form of having, such as “have” and “has”), “including” (and any form of including, such as “includes” and “include”) or “containing” (and any form of containing, such as “contains” and “contain”) are inclusive or open-ended and do not exclude additional, unrecited elements or method steps.

The term “or combinations thereof” as used herein refers to all permutations and combinations of the listed items preceding the term. For example, “A, B, C, or combinations thereof” is intended to include at least one of: A, B, C, AB, AC, BC, or ABC, and if order is important in a particular context, also BA, CA, CB, CBA, BCA, ACB, BAC, or CAB. Continuing with this example, expressly included are combinations that contain repeats of one or more item or term, such as BB, AAA, AB, BBC, AAABCCCC, CBBAAA, CABABB, and so forth. The skilled artisan will understand that typically there is no limit on the number of items or terms in any combination, unless otherwise apparent from the context.

All of the compositions and/or methods disclosed and claimed herein can be made and executed without undue experimentation in light of the present disclosure. While the compositions and methods of this invention have been described in terms of preferred embodiments, it will be apparent to those of skill in the art that variations may be applied to the compositions and/or methods and in the steps or in the sequence of steps of the method described herein without departing from the concept, spirit and scope of the invention. All such similar substitutes and modifications apparent to those skilled in the art are deemed to be within the spirit, scope and concept of the invention as defined by the appended claims.

Claims

1. A method of making polymer ammunition having a two-piece primer insert comprising the steps of:

providing a two piece primer insert comprising:
an upper primer insert portion connected to a lower primer insert portion, wherein the upper primer insert portion comprises
an upper primer insert top surface,
an upper primer insert bottom surface opposite the upper primer insert top surface,
an upper primer aperture through the upper primer insert top surface and the upper primer insert bottom surface, and
a substantially cylindrical coupling element extending away from the upper primer insert bottom surface,
wherein the lower primer insert portion comprises:
a lower primer insert bottom surface opposite a lower primer insert top surface, a primer recess in the lower primer insert top surface that extends toward the lower primer insert bottom surface and the primer recess adapted to fit a primer,
a lower flash hole aperture through the lower primer insert bottom surface, wherein the lower flash hole aperture is about the same diameter as the upper primer aperture
a groove in the lower primer insert bottom surface positioned around the lower flash hole aperture, wherein the groove is positioned between the upper primer aperture and the lower flash hole aperture, wherein the groove has a diameter greater than the lower flash hole aperture and the upper primer aperture;
providing a first polymer composition for molding a polymer ammunition cartridge;
molding from the first polymer composition a substantially cylindrical polymeric middle body having the two piece primer insert at a first end and a substantially cylindrical polymeric coupling element at a second end, wherein the first polymer composition extends over an outer surface of the two piece primer insert and extends over the substantially cylindrical coupling element through the upper primer aperture and into the groove to form a primer flash hole, wherein the first polymer composition extends from the substantially cylindrical polymeric coupling element to the primer flash hole;
forming a substantially cylindrical polymeric bullet-end component from a second polymer composition comprising a bullet aperture opposite a polymeric bullet-end coupling that mates to the substantially cylindrical coupling element;
coupling the substantially cylindrical coupling element to the polymeric bullet-end coupling to form a propellant chamber that extends from the primer flash hole aperture to the bullet aperture;
inserting a primer into the primer recess, wherein the primer is in operably communication with the propellant chamber through the primer flash hole aperture;
at least partially filling the propellant chamber with a propellant; and
frictionally fitting a projectile in the bullet-end aperture, wherein the propellant chamber is enclosed at one end by the primer and the projectile at the other end.

2. The method of claim 1, wherein an insert joint between the upper primer insert portion and the lower primer insert portion is threaded, riveted, locked, friction fitted, coined, snap fitted, chemical bonded, chemical welded, soldered, smelted, sintered, adhesive bonded, laser welded, ultrasonic welded, friction spot welded, or friction stir welded.

3. The method of claim 1, wherein the upper primer insert portion, the lower primer insert portion or both are formed independently by metal injection molding, polymer injection molding, stamping, milling, molding, machining, punching, fine blanking, smelting, or any other method that will form insert portions that may be joined together to form the two-piece primer insert.

4. The method of claim 1, wherein the upper primer insert portion, the lower primer insert portion or both independently comprise a polymer, a metal, an alloy, or a ceramic alloy.

5. The method of claim 4, wherein the upper primer insert portion and the lower primer insert portion comprise the same material or different materials.

6. The method of claim 1, wherein the upper primer insert portion comprises a polymer, a metal, an alloy, or a ceramic alloy and the lower primer insert portion comprises a different polymer, metal, alloy, or ceramic alloy.

7. The method of claim 1, wherein the upper primer insert portion and the lower primer insert portion comprise steel, nickel, chromium, copper, carbon, iron, stainless steel or brass.

8. The method of claim 1, wherein the groove in the lower primer insert bottom surface forms a flash hole groove.

9. The method of claim 1, wherein the first polymer composition, the second polymer composition or both independently comprise a nylon polymer.

10. The method of claim 1, wherein the first polymer composition, the second polymer composition or both independently comprise between about 10 and about 70 wt % glass fiber fillers, mineral fillers, or mixtures thereof.

11. The method of claim 1, wherein the first polymer composition, the second polymer composition or both independently comprise polyurethane prepolymer, cellulose, fluoro-polymer, ethylene inter-polymer alloy elastomer, ethylene vinyl acetate, nylon, polyether imide, polyester elastomer, polyester sulfone, polyphenyl amide, polypropylene, polyvinylidene fluoride or thermoset polyurea elastomer, acrylics, homopolymers, acetates, copolymers, acrylonitrile-butadinen-styrene, thermoplastic fluoro polymers, inomers, polyamides, polyamide-imides, polyacrylates, polyatherketones, polyaryl-sulfones, polybenzimidazoles, polycarbonates, polybutylene, terephthalates, polyether imides, polyether sulfones, thermoplastic polyimides, thermoplastic polyurethanes, polyphenylene sulfides, polyethylene, polypropylene, polysulfones, polyvinylchlorides, styrene acrylonitriles, polystyrenes, polyphenylene, ether blends, styrene maleic anhydrides, polycarbonates, allyls, aminos, cyanates, epoxies, phenolics, unsaturated polyesters, bismaleimides, polyurethanes, silicones, vinylesters, urethane hybrids, polyphenylsulfones, copolymers of polyphenylsulfones with polyethersulfones or polysulfones, copolymers of poly-phenylsulfones with siloxanes, blends of polyphenylsulfones with polysiloxanes, poly(etherimide-siloxane) copolymers, blends of polyetherimides and polysiloxanes, and blends of polyetherimides and poly(etherimide-siloxane) copolymers.

12. The method of claim 1, wherein the bullet aperture comprises one or more cannelures formed on an inner circumferential surface of the bullet aperture.

13. The method of claim 1, wherein the bullet aperture accepts a 0.221, 0.223, 0.243, 0.25-06, 0.264, 0.270, 0.300, 0.308, 0.338, 0.30-30, 0.30-06, 0.45-70 or 0.50-90, 50 caliber, 45 caliber, 380 caliber or 38 caliber, 5.56 mm, 6 mm, 7 mm, 7.62 mm, 8 mm, 9 mm, 10 mm, 12.7 mm, 14.5 mm, 14.7 mm, 20 mm, 25 mm, 30 mm, 40 mm, 57 mm, 60 mm, 75 mm, 76 mm, 81 mm, 90 mm, 100 mm, 105 mm, 106 mm, 115 mm, 120 mm, 122 mm, 125 mm, 130 mm, 152 mm, 155 mm, 165 mm, 175 mm, 203 mm or 460 mm, 4.2 inch or 8 inch projectile.

14. The method of claim 1, wherein the projectile has a frustoconical shaped nose.

15. The method of claim 1, further comprising the step of positioning a diffuser in the primer recess under the primer.

Referenced Cited
U.S. Patent Documents
62283 February 1867 Milbank
99528 February 1870 Boyd
113634 April 1871 Crispin
130679 August 1872 Whitmore
159665 February 1875 Gauthey
169807 November 1875 Hart
207248 August 1878 Bush et al.
462611 November 1891 Ambjorn Comte De Sparre
475008 May 1892 Bush
498856 June 1893 Overbaugh
498857 June 1893 Overbaugh
640856 January 1900 Bailey
662137 November 1900 Tellerson
676000 June 1901 Henneberg
743242 November 1903 Bush
865853 September 1907 Bailey
865979 September 1907 Bailey
869046 October 1907 Bailey
905358 December 1908 Peters
933030 August 1909 Funk
957171 May 1910 Loeb
963911 July 1910 Loeble
980351 January 1911 Sherman
1060817 May 1913 Clyne
1060818 May 1913 Clyne
1064907 June 1913 Hoagland
1187464 June 1916 Offutt
1936905 November 1933 Gaidos
1940657 December 1933 Woodford
2294822 September 1942 Albree
2465962 March 1949 Allen et al.
2654319 October 1953 Roske
2823611 February 1958 Thayer
2862446 December 1958 Lars
2918868 December 1959 Lars
2936709 May 1960 Seavey
2953990 September 1960 Miller
2972947 February 1961 Fitzsimmons et al.
3034433 May 1962 Karl
3099958 August 1963 Daubenspeck
3157121 November 1964 Daubenspeck
3159701 December 1964 Herter
3170401 February 1965 Johnson
3171350 March 1965 Metcalf et al.
3242789 March 1966 Woodring
3256815 June 1966 Davidson
3288066 November 1966 Stadler
3292538 December 1966 Hans et al.
3332352 July 1967 Olson et al.
3444777 May 1969 Lage
3446146 May 1969 Gawlick
3485170 December 1969 Scanlon
3485173 December 1969 Morgan
3491691 January 1970 Vawter
3565008 February 1971 Gulley et al.
3590740 July 1971 Herter
3609904 October 1971 Scanlon
3614929 October 1971 Herter et al.
3659528 May 1972 Santala
3688699 September 1972 Horn
3690256 September 1972 Schnitzer
3745924 July 1973 Scanlon
3749021 July 1973 Burgess
3756156 September 1973 Schuster
3765297 October 1973 Skochko
3768413 October 1973 Ramsay
3797396 March 1974 Reed
3842739 October 1974 Scanlon
3866536 February 1975 Greenberg
3874294 April 1975 Hale
3955506 May 11, 1976 Luther et al.
3977326 August 31, 1976 Anderson
3990366 November 9, 1976 Scanlon
4005630 February 1, 1977 Patrick
4007686 February 15, 1977 Hugonet
4020763 May 3, 1977 Iruretagoyena
4132173 January 2, 1979 Amuchastegui
4147107 April 3, 1979 Ringdal
4157684 June 12, 1979 Clausser
4173186 November 6, 1979 Dunham
4179992 December 25, 1979 Ramnarace
4187271 February 5, 1980 Rolston
4228724 October 21, 1980 Leich
4276830 July 7, 1981 Alice
4353304 October 12, 1982 Hubsch
4475435 October 9, 1984 Mantel
4483251 November 20, 1984 Spalding
4598445 July 8, 1986 O'Connor
4614157 September 30, 1986 Grelle
4679505 July 14, 1987 Reed
4718348 January 12, 1988 Ferrigno
4719859 January 19, 1988 Ballreich et al.
4726296 February 23, 1988 Leshner
4763576 August 16, 1988 Kass et al.
4867065 September 19, 1989 Kaltmann et al.
4958568 September 25, 1990 Buenemann
4970959 November 20, 1990 Bilsbury et al.
5021206 June 4, 1991 Stoops
5033386 July 23, 1991 Vatsvog
5063853 November 12, 1991 Bilgeri
5090327 February 25, 1992 Bilgeri
5127331 July 7, 1992 Stoops
5151555 September 29, 1992 Vatsvog
5165040 November 17, 1992 Andersson et al.
5237930 August 24, 1993 Belanger et al.
5247888 September 28, 1993 Conil
5259288 November 9, 1993 Vatsvog
5265540 November 30, 1993 Ducros
D345676 April 5, 1994 Biffle
5433148 July 18, 1995 Barratault
5535495 July 16, 1996 Gutowski
5563365 October 8, 1996 Dineen et al.
5616642 April 1, 1997 West et al.
D380650 July 8, 1997 Norris
5679920 October 21, 1997 Hallis et al.
5758445 June 2, 1998 Casull
5770815 June 23, 1998 Watson
5798478 August 25, 1998 Beal
5950063 September 7, 1999 Hens et al.
5961200 October 5, 1999 Friis
5969288 October 19, 1999 Baud
5979331 November 9, 1999 Casull
6004682 December 21, 1999 Rackovan et al.
6048379 April 11, 2000 Bray et al.
6070532 June 6, 2000 Halverson
D435626 December 26, 2000 Benini
6257148 July 10, 2001 Toivonen
6257149 July 10, 2001 Cesaroni
D447209 August 28, 2001 Benini
6272993 August 14, 2001 Cook et al.
6283035 September 4, 2001 Olson et al.
6357357 March 19, 2002 Glasser
D455052 April 2, 2002 Gullickson et al.
D455320 April 9, 2002 Edelstein
6375971 April 23, 2002 Hansen
6408764 June 25, 2002 Heitmann
6450099 September 17, 2002 Desgland
6460464 October 8, 2002 Attarwala
6523476 February 25, 2003 Riess et al.
6644204 November 11, 2003 Pierrot
6649095 November 18, 2003 Buja
6672219 January 6, 2004 Mackerell et al.
6708621 March 23, 2004 Forichon-Chaumet
6752084 June 22, 2004 Husseini et al.
6796243 September 28, 2004 Schmees
6810816 November 2, 2004 Rennard
6840149 January 11, 2005 Beal
6845716 January 25, 2005 Husseini et al.
7000547 February 21, 2006 Amick
7014284 March 21, 2006 Morton et al.
7032492 April 25, 2006 Meshirer
7056091 June 6, 2006 Powers
7059234 June 13, 2006 Husseini
7165496 January 23, 2007 Reynolds
D540710 April 17, 2007 Charrin
7204191 April 17, 2007 Wiley et al.
7213519 May 8, 2007 Wiley
7231519 June 12, 2007 Joseph et al.
7232473 June 19, 2007 Elliott
7299750 November 27, 2007 Schikora et al.
7353756 April 8, 2008 Leasure
7380505 June 3, 2008 Shiery
7383776 June 10, 2008 Amick
7392746 July 1, 2008 Hansen
7441504 October 28, 2008 Husseini et al.
D583927 December 30, 2008 Benner
7458322 December 2, 2008 Reynolds et al.
7461597 December 9, 2008 Brunn
7568417 August 4, 2009 Lee
7585166 September 8, 2009 Buja
7610858 November 3, 2009 Chung
7750091 July 6, 2010 Maljkovic et al.
D626619 November 2, 2010 Gogol et al.
7841279 November 30, 2010 Reynolds et al.
D631699 February 1, 2011 Moreau
D633166 February 22, 2011 Richardson et al.
7930977 April 26, 2011 Klein
8007370 August 30, 2011 Hirsch et al.
8056232 November 15, 2011 Patel et al.
8156870 April 17, 2012 South
8186273 May 29, 2012 Trivette
8201867 June 19, 2012 Thomeczek
8206522 June 26, 2012 Sandstrom et al.
8240252 August 14, 2012 Maljkovic et al.
D675882 February 12, 2013 Crockett
8393273 March 12, 2013 Weeks et al.
8408137 April 2, 2013 Battaglia
D683419 May 28, 2013 Rebar
8443729 May 21, 2013 Mittelstaedt
8443730 May 21, 2013 Padgett
8511233 August 20, 2013 Nilsson
D689975 September 17, 2013 Carlson et al.
8522684 September 3, 2013 Davies et al.
8540828 September 24, 2013 Busky et al.
8561543 October 22, 2013 Burrow
8573126 November 5, 2013 Klein
8641842 February 4, 2014 Hafner et al.
8689696 April 8, 2014 Seeman et al.
8763535 July 1, 2014 Padgett
8790455 July 29, 2014 Borissov et al.
8807008 August 19, 2014 Padgett et al.
8813650 August 26, 2014 Maljkovic et al.
D715888 October 21, 2014 Padgett
8850985 October 7, 2014 Maljkovic et al.
8857343 October 14, 2014 Marx
8869702 October 28, 2014 Padgett
D717909 November 18, 2014 Thrift et al.
8875633 November 4, 2014 Padgett
8893621 November 25, 2014 Escobar
8978559 March 17, 2015 Davies et al.
9003973 April 14, 2015 Padgett
9032855 May 19, 2015 Foren et al.
9091516 July 28, 2015 Davies
9103641 August 11, 2015 Nielson et al.
9157709 October 13, 2015 Nuetzman et al.
9170080 October 27, 2015 Poore et al.
9182204 November 10, 2015 Maljkovic et al.
9188412 November 17, 2015 Maljkovic et al.
9200157 December 1, 2015 El-Hibri et al.
9200880 December 1, 2015 Foren
9212876 December 15, 2015 Kostka et al.
9212879 December 15, 2015 Whitworth
9213175 December 15, 2015 Arnold
9254503 February 9, 2016 Ward
9255775 February 9, 2016 Rubin
D752397 March 29, 2016 Seiders et al.
D754223 April 19, 2016 Pederson et al.
9329004 May 3, 2016 Pace
9335137 May 10, 2016 Maljkovic et al.
9337278 May 10, 2016 Gu et al.
9347457 May 24, 2016 Ahrens et al.
9366512 June 14, 2016 Burczynski et al.
9377278 June 28, 2016 Rubin
9389052 July 12, 2016 Conroy et al.
9395165 July 19, 2016 Maljkovic et al.
D764624 August 23, 2016 Masinelli
D765214 August 30, 2016 Padgett
9429407 August 30, 2016 Burrow
9441930 September 13, 2016 Burrow
9453714 September 27, 2016 Bosarge et al.
D773009 November 29, 2016 Bowers
9500453 November 22, 2016 Schluckebier et al.
9506735 November 29, 2016 Burrow
D774824 December 27, 2016 Gallagher
9513096 December 6, 2016 Burrow
9518810 December 13, 2016 Burrow
9523563 December 20, 2016 Burrow
9528799 December 27, 2016 Maljkovic
9546849 January 17, 2017 Burrow
9551557 January 24, 2017 Burrow
D778391 February 7, 2017 Burrow
D778393 February 7, 2017 Burrow
D778394 February 7, 2017 Burrow
D778395 February 7, 2017 Burrow
D779021 February 14, 2017 Burrow
D779024 February 14, 2017 Burrow
D780283 February 28, 2017 Burrow
D781393 March 14, 2017 Burrow
9587918 March 7, 2017 Burrow
9599443 March 21, 2017 Padgett et al.
9625241 April 18, 2017 Neugebauer
9631907 April 25, 2017 Burrow
9644930 May 9, 2017 Burrow
9658042 May 23, 2017 Emary
9683818 June 20, 2017 Lemke et al.
D792200 July 18, 2017 Baiz et al.
9709368 July 18, 2017 Mahnke
D797880 September 19, 2017 Seecamp
9759554 September 12, 2017 Ng et al.
D800244 October 17, 2017 Burczynski et al.
D800245 October 17, 2017 Burczynski et al.
D800246 October 17, 2017 Burczynski et al.
9784667 October 10, 2017 Lukay et al.
9835423 December 5, 2017 Burrow
9835427 December 5, 2017 Burrow
9857151 January 2, 2018 Dionne et al.
9869536 January 16, 2018 Burrow
9879954 January 30, 2018 Hajjar
9885551 February 6, 2018 Burrow
D813975 March 27, 2018 White
9921040 March 20, 2018 Rubin
9927219 March 27, 2018 Burrow
9933241 April 3, 2018 Burrow
9939236 April 10, 2018 Drobockyi et al.
9964388 May 8, 2018 Burrow
D821536 June 26, 2018 Christiansen et al.
9989339 June 5, 2018 Riess
10041770 August 7, 2018 Burrow
10041771 August 7, 2018 Burrow
10041776 August 7, 2018 Burrow
10041777 August 7, 2018 Burrow
10048049 August 14, 2018 Burrow
10048050 August 14, 2018 Burrow
10048052 August 14, 2018 Burrow
10054413 August 21, 2018 Burrow
D828483 September 11, 2018 Burrow
10081057 September 25, 2018 Burrow
D832037 October 30, 2018 Gallagher
10101140 October 16, 2018 Burrow
10124343 November 13, 2018 Tsai
10145662 December 4, 2018 Burrow
10190857 January 29, 2019 Burrow
10234249 March 19, 2019 Burrow
10234253 March 19, 2019 Burrow
10240905 March 26, 2019 Burrow
10254096 April 9, 2019 Burrow
10260847 April 16, 2019 Viggiano et al.
D849181 May 21, 2019 Burrow
10302403 May 28, 2019 Burrow
10302404 May 28, 2019 Burrow
10323918 June 18, 2019 Menefee, III
10330451 June 25, 2019 Burrow
10345088 July 9, 2019 Burrow
10352664 July 16, 2019 Burrow
10352670 July 16, 2019 Burrow
10359262 July 23, 2019 Burrow
10365074 July 30, 2019 Burrow
D861118 September 24, 2019 Burrow
D861119 September 24, 2019 Burrow
10408582 September 10, 2019 Burrow
10408592 September 10, 2019 Boss et al.
10415943 September 17, 2019 Burrow
10429156 October 1, 2019 Burrow
10458762 October 29, 2019 Burrow
10466020 November 5, 2019 Burrow
10466021 November 5, 2019 Burrow
10480911 November 19, 2019 Burrow
10480912 November 19, 2019 Burrow
10480915 November 19, 2019 Burrow et al.
10488165 November 26, 2019 Burrow
10533830 January 14, 2020 Burrow et al.
10571228 February 25, 2020 Burrow
10571229 February 25, 2020 Burrow
10571230 February 25, 2020 Burrow
10571231 February 25, 2020 Burrow
10578409 March 3, 2020 Burrow
10591260 March 17, 2020 Burrow et al.
D882019 April 21, 2020 Burrow et al.
D882020 April 21, 2020 Burrow et al.
D882021 April 21, 2020 Burrow et al.
D882022 April 21, 2020 Burrow et al.
D882023 April 21, 2020 Burrow et al.
D882024 April 21, 2020 Burrow et al.
D882025 April 21, 2020 Burrow et al.
D882026 April 21, 2020 Burrow et al.
D882027 April 21, 2020 Burrow et al.
D882028 April 21, 2020 Burrow et al.
D882029 April 21, 2020 Burrow et al.
D882030 April 21, 2020 Burrow et al.
D882031 April 21, 2020 Burrow et al.
D882032 April 21, 2020 Burrow et al.
D882033 April 21, 2020 Burrow et al.
D882720 April 28, 2020 Burrow et al.
D882721 April 28, 2020 Burrow et al.
D882722 April 28, 2020 Burrow et al.
D882723 April 28, 2020 Burrow et al.
D882724 April 28, 2020 Burrow et al.
10612896 April 7, 2020 Burrow
10612897 April 7, 2020 Burrow et al.
D884115 May 12, 2020 Burrow et al.
D886231 June 2, 2020 Burrow et al.
D886937 June 9, 2020 Burrow et al.
10677573 June 9, 2020 Burrow et al.
D891567 July 28, 2020 Burrow et al.
D891568 July 28, 2020 Burrow et al.
D891569 July 28, 2020 Burrow et al.
D891570 July 28, 2020 Burrow et al.
10704869 July 7, 2020 Burrow et al.
10704870 July 7, 2020 Burrow et al.
10704871 July 7, 2020 Burrow et al.
10704872 July 7, 2020 Burrow et al.
10704876 July 7, 2020 Boss et al.
10704877 July 7, 2020 Boss et al.
10704878 July 7, 2020 Boss et al.
10704879 July 7, 2020 Burrow et al.
10704880 July 7, 2020 Burrow et al.
D892258 August 4, 2020 Burrow et al.
D893665 August 18, 2020 Burrow et al.
D893666 August 18, 2020 Burrow et al.
D893667 August 18, 2020 Burrow et al.
D893668 August 18, 2020 Burrow et al.
D894320 August 25, 2020 Burrow et al.
10731956 August 4, 2020 Burrow et al.
10731957 August 4, 2020 Burrow et al.
10753713 August 25, 2020 Burrow
10760882 September 1, 2020 Burrow
D903038 November 24, 2020 Burrow et al.
D903039 November 24, 2020 Burrow et al.
10845169 November 24, 2020 Burrow
10852108 December 1, 2020 Burrow et al.
10859352 December 8, 2020 Burrow
10876822 December 29, 2020 Burrow et al.
10948272 March 16, 2021 Drobockyi
20030127011 July 10, 2003 Mackerell et al.
20040074412 April 22, 2004 Kightlinger
20040200340 October 14, 2004 Robinson
20050056183 March 17, 2005 Meshirer
20050081704 April 21, 2005 Husseini
20050132922 June 23, 2005 Thiesen
20050257712 November 24, 2005 Husseini et al.
20060027125 February 9, 2006 Brunn
20060278116 December 14, 2006 Hunt
20060283345 December 21, 2006 Feldman et al.
20070056343 March 15, 2007 Cremonesi
20070181029 August 9, 2007 Mcaninch
20070214992 September 20, 2007 Dittrich
20070214993 September 20, 2007 Cerovic et al.
20070261587 November 15, 2007 Chung
20070267587 November 22, 2007 Dalluge
20100101444 April 29, 2010 Schluckebier
20100212533 August 26, 2010 Brunn
20100234132 September 16, 2010 Hirsch et al.
20100258023 October 14, 2010 Reynolds
20100282112 November 11, 2010 Battaglia
20110179965 July 28, 2011 Mason
20120024183 February 2, 2012 Klein
20120111219 May 10, 2012 Burrow
20120180685 July 19, 2012 Se-Hong
20120180687 July 19, 2012 Padgett
20120180688 July 19, 2012 Padgett
20120291655 November 22, 2012 Jones
20130008335 January 10, 2013 Menefee, III
20130014664 January 17, 2013 Padgett
20130014665 January 17, 2013 Maljkovic et al.
20130076865 March 28, 2013 Tateno et al.
20130186294 July 25, 2013 Davies
20130291711 November 7, 2013 Mason
20140224144 August 14, 2014 Neugebauer
20140260925 September 18, 2014 Beach
20140261044 September 18, 2014 Seecamp
20140311332 October 23, 2014 Carlson et al.
20150075400 March 19, 2015 Lemke
20150226220 August 13, 2015 Bevington
20150241183 August 27, 2015 Padgett
20150268020 September 24, 2015 Emary
20160003585 January 7, 2016 Carpenter et al.
20160003589 January 7, 2016 Burrow
20160003590 January 7, 2016 Burrow
20160003593 January 7, 2016 Burrow
20160003594 January 7, 2016 Burrow
20160003595 January 7, 2016 Burrow
20160003596 January 7, 2016 Burrow
20160003597 January 7, 2016 Burrow
20160003601 January 7, 2016 Burrow
20160033241 February 4, 2016 Burrow
20160102030 April 14, 2016 Coffey et al.
20160146585 May 26, 2016 Padgett
20160245626 August 25, 2016 Drieling
20160265886 September 15, 2016 Aldrich
20160349022 December 1, 2016 Burrow
20160349023 December 1, 2016 Burrow
20160349028 December 1, 2016 Burrow
20160356588 December 8, 2016 Burrow
20160377399 December 29, 2016 Burrow
20170030690 February 2, 2017 Viggiano et al.
20170030692 February 2, 2017 Drobockyi
20170080498 March 23, 2017 Burrow
20170082409 March 23, 2017 Burrow
20170082411 March 23, 2017 Burrow
20170089673 March 30, 2017 Burrow
20170089674 March 30, 2017 Burrow
20170089675 March 30, 2017 Burrow
20170089679 March 30, 2017 Burrow
20170115105 April 27, 2017 Burrow
20170153093 June 1, 2017 Burrow
20170153099 June 1, 2017 Burrow
20170191812 July 6, 2017 Padgett
20170199018 July 13, 2017 Burrow
20170205217 July 20, 2017 Burrow
20170261296 September 14, 2017 Burrow
20170261299 September 14, 2017 Burrow
20170299352 October 19, 2017 Burrow
20180066925 March 8, 2018 Skowron et al.
20180106581 April 19, 2018 Rogers
20180224252 August 9, 2018 O'Rourke
20180224253 August 9, 2018 Burrow
20180224256 August 9, 2018 Burrow
20180259310 September 13, 2018 Burrow
20180292186 October 11, 2018 Padgett et al.
20180306558 October 25, 2018 Padgett et al.
20190011232 January 10, 2019 Boss et al.
20190011233 January 10, 2019 Boss et al.
20190011234 January 10, 2019 Boss et al.
20190011235 January 10, 2019 Boss et al.
20190011236 January 10, 2019 Burrow
20190011237 January 10, 2019 Burrow
20190011238 January 10, 2019 Burrow
20190011239 January 10, 2019 Burrow
20190011240 January 10, 2019 Burrow
20190011241 January 10, 2019 Burrow
20190025019 January 24, 2019 Burrow
20190025020 January 24, 2019 Burrow
20190025021 January 24, 2019 Burrow
20190025022 January 24, 2019 Burrow
20190025023 January 24, 2019 Burrow
20190025024 January 24, 2019 Burrow
20190025025 January 24, 2019 Burrow
20190025026 January 24, 2019 Burrow
20190025035 January 24, 2019 Burrow
20190025036 January 24, 2019 Burrow
20190078862 March 14, 2019 Burrow
20190106364 April 11, 2019 James
20190107375 April 11, 2019 Burrow
20190137228 May 9, 2019 Burrow et al.
20190137229 May 9, 2019 Burrow et al.
20190137230 May 9, 2019 Burrow et al.
20190137231 May 9, 2019 Burrow et al.
20190137232 May 9, 2019 Burrow et al.
20190137233 May 9, 2019 Burrow et al.
20190137234 May 9, 2019 Burrow et al.
20190137235 May 9, 2019 Burrow et al.
20190137236 May 9, 2019 Burrow et al.
20190137237 May 9, 2019 Burrow et al.
20190137238 May 9, 2019 Burrow et al.
20190137239 May 9, 2019 Burrow et al.
20190137240 May 9, 2019 Burrow et al.
20190137241 May 9, 2019 Burrow et al.
20190137242 May 9, 2019 Burrow et al.
20190137243 May 9, 2019 Burrow et al.
20190137244 May 9, 2019 Burrow et al.
20190170488 June 6, 2019 Burrow
20190204050 July 4, 2019 Burrow
20190204056 July 4, 2019 Burrow
20190212117 July 11, 2019 Burrow
20190242679 August 8, 2019 Viggiano et al.
20190242682 August 8, 2019 Burrow
20190242683 August 8, 2019 Burrow
20190249967 August 15, 2019 Burrow et al.
20190257625 August 22, 2019 Burrow
20190310058 October 10, 2019 Burrow
20190310059 October 10, 2019 Burrow
20190316886 October 17, 2019 Burrow
20190360788 November 28, 2019 Burrow
20190376773 December 12, 2019 Burrow
20190376774 December 12, 2019 Boss et al.
20190383590 December 19, 2019 Burrow
20200011645 January 9, 2020 Burrow et al.
20200011646 January 9, 2020 Burrow et al.
20200025536 January 23, 2020 Burrow et al.
20200025537 January 23, 2020 Burrow et al.
20200033102 January 30, 2020 Burrow
20200033103 January 30, 2020 Burrow et al.
20200041239 February 6, 2020 Burrow
20200049469 February 13, 2020 Burrow
20200049470 February 13, 2020 Burrow
20200049471 February 13, 2020 Burrow
20200049472 February 13, 2020 Burrow
20200049473 February 13, 2020 Burrow
20200056872 February 20, 2020 Burrow
20200109932 April 9, 2020 Burrow
20200149853 May 14, 2020 Burrow
20200158483 May 21, 2020 Burrow
20200200512 June 25, 2020 Burrow
20200200513 June 25, 2020 Burrow
20200208948 July 2, 2020 Burrow
20200208949 July 2, 2020 Burrow
20200208950 July 2, 2020 Burrow
20200225009 July 16, 2020 Burrow
20200248998 August 6, 2020 Burrow
20200248999 August 6, 2020 Burrow
20200249000 August 6, 2020 Burrow
20200256654 August 13, 2020 Burrow
20200263967 August 20, 2020 Burrow et al.
20200278183 September 3, 2020 Burrow et al.
20200292283 September 17, 2020 Burrow
20200300587 September 24, 2020 Burrow et al.
20200300592 September 24, 2020 Overton et al.
20200309490 October 1, 2020 Burrow et al.
20200309496 October 1, 2020 Burrow et al.
20200326168 October 15, 2020 Boss et al.
20200363173 November 19, 2020 Burrow
20200363179 November 19, 2020 Overton et al.
20200378734 December 3, 2020 Burrow
20200393220 December 17, 2020 Burrow
20200400411 December 24, 2020 Burrow
20210003373 January 7, 2021 Burrow
20210041211 February 11, 2021 Pennell
20210108898 April 15, 2021 Overton
Foreign Patent Documents
2813634 April 2012 CA
102901403 June 2014 CN
16742 January 1882 DE
2625486 August 2017 EP
1412414 October 1965 FR
783023 September 1957 GB
2172467 August 2001 RU
0034732 June 2000 WO
2007014024 February 2007 WO
2012047615 April 2012 WO
2012097320 July 2012 WO
2012097317 November 2012 WO
2013070250 May 2013 WO
2013096848 June 2013 WO
2014062256 April 2014 WO
2016003817 January 2016 WO
2019094544 May 2019 WO
2019160742 August 2019 WO
Other references
  • AccurateShooter.com Daily Bulletin “New PolyCase Ammunition and Injection-Molded Bullets” Jan. 11, 2015.
  • International Ammunition Association, Inc. website, published on Apr. 2017, PCP Ammo Variation in U.S. Military Polymer/Metal Cartridge Case R&D, Available on the Internet URL https://forum.cartridgecollectors.org/t/pcp-ammo-variation-in-u-s-military-polyer-metal-cartridge-case-r-d/24400.
  • International Search Report and Written Opinion for PCTUS201859748 dated Mar. 1, 2019, pp. 1-9.
  • International Search Report and Written Opinion for PCTUS2019017085 dated Apr. 19, 2019, pp. 1-9.
  • Korean Intellectual Property Office (ISA), International Search Report and Written Opinion for PCT/US2011/062781 dated Nov. 30, 2012, 16 pp.
  • Korean Intellectual Property Office (ISA), International Search Report and Written Opinion for PCT/US2015/038061 dated Sep. 21, 2015, 28 pages.
  • Luck Gunner.com, Review: Polymer Cased Rifle Ammunition from PCP Ammo, Published Jan. 6, 2014, Available on the Internet URL https://www.luckygunner.com/lounge/pcp-ammo-review.
  • YouTube.com—TFB TV, Published on Jul. 23, 2015, available on Internal URL https://www.youtubecom/watch?v=mCjNkbxHkEE.
  • International Search Report and Written Opinion in PCT/US2019/040323 dated Sep. 24, 2019, pp. 1-16.
  • International Search Report and Written Opinion in PCT/US2019/040329 dated Sep. 27, 2019, pp. 1-24.
  • International Preliminary Report on Patentability and Written Opinion in PCT/US2018/059748 dated May 12, 2020; pp. 1-8.
  • International Search Report and Written Opinion in PCT/US2020/023273 dated Oct. 7, 2020; pp. 1-11.
  • IPRP in PCT2019017085 dated Aug. 27, 2020, pp. 1-8.
Patent History
Patent number: 11098990
Type: Grant
Filed: Feb 18, 2019
Date of Patent: Aug 24, 2021
Patent Publication Number: 20190212117
Assignee: TRUE VELOCITY IP HOLDINGS, LLC (Garland, TX)
Inventor: Lonnie Burrow (Carrollton, TX)
Primary Examiner: Derrick R Morgan
Application Number: 16/278,499
Classifications
Current U.S. Class: With Primer Means (102/470)
International Classification: F42B 5/30 (20060101); F42B 5/307 (20060101); F42B 5/313 (20060101); F42C 19/08 (20060101);